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Russian and Soviet Fighter Jets and their capabilities.

Russian Fighter Jets 


Su-57 Felon Series 

Su-57S

Concept: 1998

Designed: 2004

Prototype: 2010

Completed: 2018

Production: 2021

Service: 2024

Aircraft Role: MultiRole/Air Superiority 

Generation: 5th 

Combat Rank: S

Number Made: 60+


Su-57M

Prototype: 2022

Aircraft Role: MultiRole/Air Superiority 

Generation: 5+

Combat Rank: D

Number Made: 1


Engines and Airframe: CAD composite construction LO Airframe with an RCS minimum of 0.01m². Crew of 1. Length 20 m. Height 4.6 m. Wingspan 14.1 m. Wing area 79 m². Frame weight 18,500 kg. Takeoff weight 40,000 kg. Max Fuel 10,300 kg. 2× Lyul'ka-Saturn AL-41-F1 low visibility 3D thrust vectoring variable bypass axial flow FADEC turbofans with supercruise with 177 kN thrust and 284 kN in afterburner. In flight refueling.


Speed and Endurance: Combat Range of 900-1300 km. Top speed of mach 2.2 to 2.4 at 15 km+, mach 2 to 2.2 at 10 km+, mach 1.8 to 2 to at 5 km+ and mach 1 to 1.3 at sea level with supercruise at mach 1.2 at sea level and mach 1.6 at 5 km+. Service Ceiling of 20 to 23 km. Acceleration 9-12 seconds to mach 1 at sea level. Stall speed 100-120 kph. Take off distance is 300m with ATA payload to 700m for full payload. Landing distance 500 to 700m. 


(M model adds 2× Lyul'ka-Saturn AL-51-F1 low observability 3D thrust vectoring variable bypass axial flow FADEC turbofans with supercruise with 214 kN of thrust and 332 kN in afterburner enabling Top speed of mach 2.6 to 2.8 at 15 km+, mach 2.2 to 2.4 at 10 km+, mach 2 to 2.2 to at 5 km+ and mach 1.4 to 1.8 at sea level with supercruise at mach 1.6 at sea level and mach 2 at 5 km+)


Manuvarabilities: 3D thrust vectoring with ±15° in roll/yaw and ±8° in pitch with deflection at 60 deg/s. Thrust to weight ratio of 1.3 at full air to air payload and 1.5 at half fuel/loadout and 1 at full load/fuel. Roll rate of 200 deg/s at high speed and 300 deg/s at low speed. 4× LERXs with pitch of ±60° and 2× LEVCONs with pitch of ±90° and 2× elevators with pitch of -90°. Climb rate of 300-350 m/s. No AOA limit at any speed. 3 to 12 kph/s speed bleed at high g instantaneous maneuvers and 5 to 8 kph/s speed bleed at high g sustained maneuvers. Wing loading at 350-390 kg/m². Sustained G tolerance of 10g with an Overload Tolerance of 13g and wing break at 19.5-26g.


(M model adds AL-51-F1 turbofans with 3D thrust vectoring with ±30° in roll/yaw and ±8° deg/s in pitch with deflection at 60 deg/s. Thrust to weight ratio of 1.5 at full air to air payload and 1.7 at half fuel/loadout and 1.1 at full load/fuel.)


Aircraft Turn Rates 


Sustained turn rates 


Mach 1.5> Speeds 

● 9-10 deg/s at 10 km altitude 

● 11-13 deg/s at 5 km altitude 

● 13-16 deg/s at sea level 


Mach 1> Speeds 

● 17-18 deg/s at 10 km altitude 

● 20-22 deg/s at 5 km altitude 

● 22-25 deg/s at sea level 


Mach 0.5> Speeds 

● 26-28 deg/s at 10 km altitude 

● 29-32 deg/s at 5 km altitude 

● 34-38 deg/s at sea level  


Instantaneous turn rates 


Mach 1.5> Speeds 

● 18-19 deg/s at 10 km altitude 

● 21-23 deg/s at 5 km altitude 

● 25-28 deg/s at sea level  


Mach 1> Speeds 

● 24-26 deg/s at 10 km altitude 

● 27-30 deg/s at 5 km altitude 

● 33-37 deg/s at sea level  


Mach 0.5> Speeds 

● 35-38 deg/s at 10 km altitude 

● 40-44 deg/s at 5 km altitude 

● 49-54 deg/s at sea level 


Stealth: LPI capable radar altimeter and fire control radar. low observability communication system. Airframe has Full RAM coatings, treated leading edge trails, half slanted ducts with radar blockers, low visibility airframe, internal weapon bay and thermal signature reduction. Low observability IFF. 


Airframe RCS

RCS Minimum: 0.01m²

RCS Median: 0.05m²

RCS Average: 0.1-1m²


Flight Control: SUU-50 fully computerised flight control system with a SAU-50S 6× axis computerised autopilot and a KSU-50 fully digital fly by wire AFCS utilising a 64x bit digital ADC. MFI-25Sh 5th Generation cockpit with 1× UHD LCD MFD and HOTAS control stick. ZSh-10 Flight Helmet. 


Navigation: PrNK-50 fully computerised nav/attack suite with IVS-50 fully digital navigation system utilising a BINS-SP2M 64x bit fully digital navigation computer using a fully digital INS utilising a ring laser gyroscope, hemispherical resonator gyroscope and fiber optic gyroscope with an accuracy of 0.005° in pitch, yaw and heading with a position error rate of <0.005 km/ph and velocity error rate of <0.1 m/s with a hybridised position accuracy of 1m. ARK-35 fully digital ADF. RV-25 fully digital radar altimiter. RSBN-85VM Vstrecha-M fully digital radio navigation system with DVOR and ILS with a position accuracy of <10m and angular accuracy of ±0.01°. N036 fully digital navigation radar. PPA-S/V-KNS GLONASS-K Global navigation satellite system with a max CEP of 60cm and average CEP of 3m (When inside former USSR airspace SDCM GNSS augmentation improves precision with a max CEP of 10cm and average CEP of <1m)  


Fire Control: Sh-121 fully computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with fully digital sensors with full stability augmentation with a MIRES individual modality sensor fusion system with C4I, NAV, RDR, IRST, EOT, HMD, TDL, IFF, RHAWS, RFCM, IRCM, MAW, ESM and ECM information displayed on one screen with full targeting fusion utilising the RLPK-50 radar and ATOLL electro optical, laser and infrared imaging/tracking targeting systems with a SOLO-21 fully digital FCC utilising Elbrus-8S 64x bit 8× core CPUs performing 30-40b IPS and 300-500b FLOPS. N036 Byelka 5th Generation Radar utilising a mechanically and electronically steered multi positional fully digital X/L band AESA system with slotted planar, quad radiator and patch antenna arrays using a sensor fused system with programmable fully digital signal processing with digital beam forming, coherent doppler filtering and signal modulation based LDSD with pulse doppler IFF, tactical & missile data link and SATCOM integration with CW illumination for SARH guidance, very low false alarm rates, BIST system and fully computerised radar image displaying with simultaneous multi-mode operation, simultaneous searching tracking and guidance, radar map freezing, raid assessment, active jamming, cyber warfare, predictive flight path, non tracked target tracking, adaptive processing, automatic target recognition, multi target air and ground based SAR, JEM, RCS and HRRP non cooperative target recognition functions and agile beam, raster, palmer, conical, sector, circular and spiral scan scanning modes utilising DBS, I/SAR, RBGM, GTD, MGMTT, TAR, TFR, STI and MGMTI air to ground radar modes, FTT, I/SAR, SSD and SSTT air to sea modes and SRC/LDSD, MR, LPIR, ATC, STTR, MTTR and HMD, LDR, IRST, EOT and multi target RFR based ACMs air to air radar modes with gain modulation, notch filtering, sidelobe suppression, polarization filtering, tunable frequency filters, dual band, frequency hopping, home on jam, jammer identification and phase coded pulse compression ECCM with 3,516 total GaAs & GaN T/R modules and 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance and 1 channel for sidelobe suppression and ECM with a noise factor of 3 dB with 4× X band and 8× L band antennas with 1× N036-1-01 slotted planar X band nose radar array with 1642 GaAs T/R modules with a 900 mm diameter size and HPRF power output on average being 10 kW with a 20 kW max output, 2× N036B-1-01 slotted planar X band cheek radar arrays with 802 GaAs T/R modules with each radar being ~400×150 mm in size with HPRF power output on average being 3 kW with a 10 kW max output, N036Kh patch antenna X band rear radar array with 1000 GaN T/R modules with a ~700×300 mm antenna size with HPRF power output on average being 5 kW with a 15 kW max output, 4× N036L-1-01 quad radiator antenna L band wing radar arrays with 48 GaAs T/R modules with each radar being ~1100×100 mm in size and 4× N036L-1-02 quad radiator antenna L band wing radar arrays with 24 GaAs T/R modules with each radar being ~300×100 mm in size with HPRF power output on average being 12 kW with a 60 kW max output with a 30 kW total average and total 105 kW max output for whole system. ZSh-10B Helmet with NSTsI-50 3rd Generation HMD utilising automatic cueing for targeting with image intensification, navigation data and weapons management data displayed for viewing with FLIR and electro optical data generated by aircraft sensors displayed on device screen with head and eye tracking. 5th Generation Radar display with an SVD system utilising a high resolution full colour raster image displayed on a LCD MFD with computerised target generation, ECM resolution, navigation data and aircraft flight information with data link integration. ShKAI-2M1 5th Generation HUD with a fully digital LCD glass display utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with an integrated digital bombing complex utilising gun, bomb and rocket CCRP and CCIP with gun EEGS and a digital MFD with electro optical slaving, mission control, navigation systems and weapons functions. 101KS-V multi-channel fully digital EOTS with a UHD resolution TV sight with a ~1440p day time image resolution, 1.06 μm Nd:YAG auto adjusting laser targeting system with laser rangefinding, laser designation and laser spot tracking and a 3rd Generation IRST & 3rd Generation FLIR system utilising a LN² cooled infrared imaging SWIR & LWIR InGaAs QWIP detector with an FPA format of 640x512 and a thermal image resolution of 1280×1024p. TsVB-54 fully digital ballistic computer utilising a KOMDIV-64 64x bit 2× core CPU enabling fully digitised automatic digital target lead and gun and missile coursing with gun, rocket and bomb CCRP and CCIP with a bomb and rocket accuracy of <3-5m CEP at a range up to 2000m and altitudes up to 5000m and <30-40m CEP at a range up to 10,000m and altitude up to 12,000m. 


(Prototypes used OLS-50 multi-channel fully digital EOTS with a FHD resolution TV sight with a ~1080p day time image resolution, 1.06 μm Nd:YAG auto adjusting laser targeting system with laser rangefinding, laser designation and laser spot tracking and a 3rd Generation IRST & 3rd Generation FLIR system utilising a LN² cooled infrared imaging HgCdTe detector with an FPA format of 320x240 and a thermal image resolution of 640×480p)


Communication & C2: S-111 fully digital unified communication complex with a BKS-57 fully digital software defined VHF/UHF and HF radio with 2 way communication, FM and AM receiving, built in IAD, satellite communications, low observability communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding, rekeying encryption, amplitude and phase shift keying, pulse code modulation and full digital data encryption with text, video, image and voice formats utilised operating on 99 programmable channels and 512 frequency carriers with data transfer speeds of 10 mbit/s, 1.2 gbit/s, 2 gbit/s and 8 gbit/s utilising an PPCh-B integrated FHSS and CRNG system utilising up to 20,000 frequency hops per second and 12 round cryptographic encryption for 128 bit, 14 round cryptographic encryption for 192 bit and 16 round cryptographic encryption for 256 bit with an operating LOS communication range of 600 km and BLOS up to unlimited with satellite link and the OSNOD fully digital tactical data link linked to the NDMC NTsUO military command center utilising the YeESU-TZ military C4 network that organises coordination between the Kavkaz-EASS military C3I radio communication network, Voiska PVO-PRO air defence network, ASUNO-S artillery network, PTK and Svod blue force tracking networks, Glaz-Groza UAV network and the Bylina electronic warfare network with links to BARS, Orbita, Andromeda-D, Strelets-M, Sagittarius-M, Akatsiya-E, Akatsiya-M, Barnaul-T, Baikal-1ME, Universal-1E, Fundament-M and Polyana-D4M1 C2 softwares and VIP-117M3, Lvin, 4RT-S, Legend, Planet, Type-1B, Kulon-V and Baget-K data terminals with two way communication, low observability data exchange, weapons management, radio communication integration, navigation data, IFF integration, SATCOM integration, fullly digital data encryption, ECM resistance, multi aircraft link, multi platform subscription, frequency hopping, electronic countermeasure support and C4 integration utilising ground, air and sea based computer, radar and electro optically generated data exchange with high resolution text, image, and pre recorded sound formats used with live video and voice formats displayed on tactical display, with data transfer speeds of 1024 bit/s, 2048 bit/s, 40 kbit/s, 100 kbit/s and 34.4 mbit/s every 0.5 to 1 seconds operating on 300 MHz to 3 GHz with up to 80,000 frequency hops per second on 60 frequency carriers enabling a LOS data transmission range up to 500 km and BLOS up to 1500 km and unlimited range with satellite link with data exchange between up to 1800 subscribers and unlimited with satellite link. IMA-BK fully digital FMC utilising 1888TX018 64x bit 8× core CPUs performing 30-40b IPS and 400-500b FLOPS utilising the BagrOS-4000 4-5m SLOC RTOS using an ICS-57 C4ISR suite linked to the YeESU-TZ military C4 network with company to regimental level blue force tracking software, cyber warfare systems, SATCOM integration, GNSS integration, weapons management software, electronic warfare systems, electronic countermeasure support, moving map display, integrated aircraft health management software, precision targeting, reconnaissance software, data sharing and high level C2 software. 


(M model adds improved FCS with SOLO-21 all digital FCC utilising Elbrus-32S 64x bit 32× core processors, with improved S-112 comm system and data link, new communication systems and new computers with new IMA-BKM fully digital FMC utilising Elbrus-32S 64x bit 32× core CPUs performing 60-80b IPS and 0.8-1.2t FLOPS. AI integration)


Targeting Systems: N036-1-01 X band nose AESA radar system with a horizontal scan range of 120° and a ±60° vertical scan range enabling tracking of up to 60 targets and data linking of 16 missiles with an Rmax range up to 500 km, in 15-24° STTR narrow beam mode detection range is 350 to 420 km vs RCS of 1m², 250 to 300 km vs RCS of 0.1m² and 60 to 90 km vs RCS of 0.001m², normal detection range 400 km for an aircraft with an RCS of 3m² and track range of 200 km for an aircraft with an RCS of 1m² with a LDSD detection range of 300 km for 3m² and a LDSD track range of 200 km for an aircraft with an RCS of 1m² with a rangefinding radar gun engagement range up to 20 km with a max ground attack detection range up to 400 km and a track range for tank sized targets up to 120 km with tracking of 4 targets with ground mapping up to 300 km, with base image resolutions of 0.5, 1 and 2 m at a spatial resolution size of 100, 200 and 300 km with radar imaging complete in 20 seconds, with an tracking scan range up to 120° in azimuth and ±60° in elevation with a full scan sweep in 0.2 seconds with max tracking target velocity at over 7408 kph and LPI target acquisition with over 1000 frequency hops per second and a max LPI engagement range of 200 km vs RCS of 1m², stores tracking information for up to 30 non tracked targets with predictive flight paths for non tracked targets up to 20 seconds with LDSD ground clutter rejection of 130> dB, NCTR for 8 targets up to 80> km with a scan range of ±60° in azimuth and ±30° in elevation with up to 400 preprogrammed target identifiers and very high chaff rejection with a MTBF of 1000 to 1500 hours. N036B-1-01 X band AESA side radars with a horizontal scan range of 120°  and ±60° vertical scan range enabling tracking of up to 60 targets and data linking of 16 missiles with an Rmax range up to 200 km, 90 to 120 km detection range for an aircraft with an RCS of 1m² to 3m² and track range of 60 km for an aircraft with an RCS of 1m² with a LDSD detection range of 100 km for 3m² and a LDSD track range of 120 km for an aircraft with an RCS of 1m² with an tracking scan range of 120° in azimuth and ±60° in elevation with a full scan sweep in 0.2 seconds with max tracking target velocity at over 7408 kph and LPI target acquisition with over 500 frequency hops per second and a max LPI engagement range of 60 km vs RCS of 1m² and stores tracking information for up to 30 non tracked targets with predictive flight paths for non tracked targets up to 20 seconds with LDSD ground clutter rejection of 130> dB, NCTR for 8 targets up to 80> km with a scan range of ±60° in azimuth and ±30° in elevation with up to 400 preprogrammed target identifiers and very high chaff rejection with a MTBF of 1000 to 1500 hours. N036Kh rear radar with a horizontal scan range of 120° and a ±60° vertical scan range enabling tracking of up to 60 targets and data linking of 16 missiles with an Rmax range up to 350 km, 300 km detection range for an aircraft with an RCS of 3m² and track range of 120 km for an aircraft with an RCS of 1m² with a LDSD detection range of 200 km for 3m² and a LDSD track range of 120 km for an aircraft with an RCS of 1m² with an tracking scan range up to 120° in azimuth and ±60° in elavasion with a full scan sweep in 0.2 seconds with max tracking target velocity at over 7048 kph and LPI target acquisition with over 1000 frequency hops per second and a max LPI engagement range of 120 km vs RCS of 1m² and stores tracking information for up to 30 non tracked targets with predictive flight paths for non tracked targets up to 20 seconds with LDSD ground clutter rejection of 130> dB, NCTR for 8 targets up to 80> km with a scan range of ±60° in azimuth and ±30° in elevation with up to 400 preprogrammed target identifiers and very high chaff rejection with a MTBF of 1000 to 1500 hours. N036L-1-01/02 radars with a horizontal scan range of 300° scan range with tracking of 60 targets with a 500 km Rmax range, 400 km detection range for 3m² and 150 km track range for 0.1 m². X/L band Radar Data fused targeting with a horizontal scan range of 360° and a ±60° vertical scan range enabling tracking of up to 60 targets and data linking of 16 missiles with an Rmax range up to 500 km, 400 km detection range for an aircraft with an RCS of 3m² and track range of 200 km for an aircraft with an RCS of 0.1m², for side system with an Rmax range up to 400 km, 200 to 400 km detection range for an aircraft with an RCS of 1m² to 5m² and track range of 100-200 km for an aircraft with an RCS of 0.01-1m² with max tracking target velocity at over 7408 kph and LPI target acquisition with over 1000 frequency hops per second and a max LPI engagement range of 200 km vs RCS of 1m², stores tracking information for up to 30 non tracked targets with predictive flight paths for non tracked targets up to 20 seconds with LDSD ground clutter rejection of 130> dB, NCTR for 8 targets up to 80> km with a scan range of ±60° in azimuth and ±30° in elevation with up to 400 preprogrammed target identifiers and very high chaff rejection with a MTBF of 1000 to 1500 hours. 101KS-V fully stabilised sight with a fully digital electro optical system with a 1× optical magnification with an FOV of 75° and a 10× optical magnification with an FOV of 7.5° with an independent stabilised vertical movement of -15°/+60° and independent stabilised horizontal movement of 180° with a moving stabilisation accuracy of 0.05 mils in azimuth and elevation and minimum/maximum stabilised sight movements of 0.03/60 deg/s with an angular tracking rate of 40 to 60 deg/s with FLIR enabling a max range of 30 km, detection of tank sized targets up to 12 km and identification up to 3 km with detection of corvette sized warships up to 28 km with identification up to 20 km with detection of fighter sized targets up to 20 km and identification up to 4 km, TV sight enabling a max range of 20 km, detection of tank sized targets up to 13 km and identification up to 10 km with detection of fighter sized targets up to 16 km and identification up to 14 km with NFOV detection of corvette sized warships up to 18 km with identification up to 15 km with automatic target tracking up to 8 km, IRST with automatic target tracking, automatic target slaving and automatic target recognition with tracking of up to 400 targets with an angular resolution of 0.01° and max target tracking rate of 300 deg/s enabling a max range up to 250 km with a 190 to 230 km detection range and 120 to 170 km rear track range with 90 km front track range for fighter sized targets and a 80 km track range for ground targets with a laser targeting system using laser rangefinding, laser designation and laser spot tracking with an accuracy of 3m with a 30 km engagement range for aircraft and 40 km engagement range for ground targets. 101KS-P FLIR with detection of tank sized targets up to 11 km and an identification range up to 3 km. NSTsI-50 HMD with an all aspect FOV and engagement range up to 50 km. 


Targeting Pods 


101KS-N Atoll-N 3rd Generation Targeting Pod with UHD EOTS with a ~1440p day time image resolution, Raduga-V 3rd Generation FLIR system utilising a 1PN136 matrix with a 388x384 FPA format, 776×768p thermal image resolution, 3-5 μm spectral range, pixel pitch of 15 μm, NETp of 30 mK and 50 Hz refresh rate with an integrated auto adjusting Nd:YAG laser targeting system with laser rangefinding, laser designation and laser spot tracking with an accuracy of 10m with utilising a fully digital telescopic electro optical sight with a day time 4× optical magnification with an FOV of 25°, 60× optical magnification with an FOV of 1.6° and a 120× electro optical magnification with an FOV of 0.8° with a night time 1× optical magnification with an FOV of 24°, 10× optical magnification with an FOV of 2.4° and a 20× optical magnification with an FOV of 1.2° with independent stabilised depth movement, an independent stabilised vertical movement of -170°/+10° and independent stabilised horizontal movement of 180° with a moving stabilisation accuracy of ±0.05 in elevation and azimuth and minimum/ maximum stabilised sight movements of 0.01/60 deg/s with an angular tracking rate of 50 to 90 deg/s with tracking of up to 30 targets and locking of up to 8 with FLIR enabling a max range of 30 km, detection of tank sized targets up to 12 km and identification up to 3 km with detection of corvette sized warships up to 28 km with identification up to 20 km with detection of fighter sized targets up to 20 km and identification up to 4 km with automatic target tracking up to 8km, TV sight enabling a max range of 90 km, detection of tank sized targets up to 50 km and identification up to 45 km with detection of fighter sized targets up to 70 km and identification up to 60 km with detection of corvette sized warships up to 87 km with identification up to 80 km with a 40 km laser engagement range for ground targets. 


Counter Measures: L-150-400/SPO-32M Pastel-M 4th Generation fully digital sensor fused RHAWS with 20 targets tracked with 300> preprogrammed threat identifiers with guidance of up to 8 ARMs with 4 fired simultaneous with 16× receivers enabling a self protection envelope of 360° in azimuth and elevation with band coverage of 0.2-20 GHz with a signal detectability range up to 500 km. Type 4283MP/Type 4280MD fully digital low observability IFF interrogator/transponder linked to the Password-3 fully digital IFF system with aircraft ID, low observability data sharing, satellite navigation locating, full digital data encryption, reprogramming and cryptographic encoding. 6× 101KS-U UV MAW and laser warning receivers covering a spectral range of 0.1 to 0.4 µm for MAW and covering a pulse repetition frequency of 0.1 to 70 Hz and pulse duration of 60 ks and spectral range of 0.9 to 1.7 µm for LWR enabling a protection envelope of 360° in azimuth and ±180° in elevation with a launch detection range of 100 km> and course trajectory detection range of <12 km. 2× 101KS-O IR MAW receivers covering a spectral range of 3 to 5 µm with a launch detection range of 100 km> and course trajectory detection range of 10> km with integrated 3rd Generation IRCM transmitters utilising laser based DIRCM with an engagement range of 10 km> and minimum system response in <2 seconds with a self protection envelope of 360° in azimuth and ±180° in elevation. UV-50-01 countermeasure dispensers utilising 2nd Generation IRCM and 3rd Generation RFCM with 84 total rounds using PPR-50-17-110V composite aluminium jammer assisted chaff that activates in 0.3 seconds and creates a false target RCS of greater than 60m², PPI-50-3 spectral flare with a minimum burn time of 3 seconds and Lobushka disposable DRFM jammers with a jamming time up to 6 seconds. K-36D-5 Zero-Zero ejection seat. SOZhE fully digital ICAS with full ECLSS and fire countermeasure system. Blesna Diamant-S 3rd Generation RFCM with a towed decoy SPJ with a 100m towing range utilising simultaneous LPIR, monopulse, continuous wave and pulse doppler countermeasure. 


Electronic Warfare: L-402 Himalayas 5th Generation fully digital ECM System with an SPJ suite utilising radio direction finder with AoA and PRF determination, simultaneous monopulse countermeasure, continuous wave countermeasure, pulse doppler countermeasure and LPIR countermeasure with doppler shifting, noise cloaking, home on jam, anti burn though and self jam resistance ECCM with track breaker, advanced decoy generation, blip enhancement, cyber warfare suite, interferometry, spectrum analyzer, counter SIGINT, satellite interception and global navigation spoofing ELINT with 8× receivers enabling a passive ECCM protection envelope of 360° in azimuth with a self protection jamming range of 400 km> with an active jamming system operating on 2-20 GHz with frequency agile deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, spot jamming, wave jamming, power managed jamming and DRFM/ISRJ jamming ECM with 1× GaN AESA patch antenna, 3× GaAs AESA planar antenna and 8× GaAs AESA quad radiator antenna ECM transmitters with an active jamming range of 500 km> 


Guns: GSh-30-1M 30mm autocannon with an effective firing range up to 2 km slaved to HMD, laser rangefinder and radar. 


Ordinance Capacity: 12× hardpoints with 4× large internal and 2× small internal and 6× external with a max 10,000 kg munition capacity and with 150 rounds for gun.  


Common Internal Air to Air Payloads

4x R-97 2x R-74M2

6× R-77M 2x R-74M2

2x R-97 3x R-77M 2x R-74M2

1× R-37M 2× R-77M 2× R-74M2

2× R-37M 2× R-74M2


Non Stealth Air to Air Payloads 

● 4× AKU-620 racks with R-37M 4× R-77M internal 2× R-74M2 internal 

● 6× AKU-170M dual racks with R-77M 4× R-97 internal 2× R-74M2 internal 


R-77M

5th Generation Radar Missile 

9B-1103M2 Ka/Ku band AESA Active Seeker with 64 GaAs T/R modules using an fully digital patch antenna array with an INS/GNSS utilising a bi-directional radio correction data link with back up inertial operting guidance, LPIR, home on jam, dual band seeker and polarisation filtering ECCM utilising a solid fuel dual pulse rocket motor with a laser and radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~300 km max Range at 10 km+ 

~250 km max Range at 5 km+

~150 km max Range at sea level 

~120 km engagement range vs RCS of 1m² at sea level 

~190 km engagement range vs RCS of 1m² at 5 km+ altitude 

~220 km engagement range vs RCS of 1m² at 10 km+ altitude 

~50 km NEZ range vs RCS of 1m² at sea level 

~70 km NEZ range vs RCS of 1m² at 5 km> altitude

~90 km NEZ range vs RCS of 1m² at 10 km> altitude 

~2 km ARH lock range vs RCS of 0.003m²

~14 km ARH lock range vs RCS of 1m²

~26 km ARH lock range vs RCS of 3m²

~35 km ARH lock range vs RCS of 10m²

~0.0005 m² minimum target RCS for ARH lock 

~Mach 6 max target velocity 

~Mach 5 top speed above 5 km altitude 

~Mach 3 top speed at sea level

~Targeting Angles 60°

~Turn Rate 70 to 120 Deg/s

~Initial Acceleration of 300-600 m/s>

~Launch limiter 10g 

~Target limiter 12g 

~Overload Tolerance 80g


R-97 

5th Generation Radar Missile 

9B-1103M1 Ka/Ku band AESA Active Seeker with 76 GaAs T/R modules using an fully digital slotted planar antenna array with an INS/GNSS utilising a bi-directional radio correction data link with back up inertial operting guidance, LPIR, home on jam, dual band seeker and polarisation filtering ECCM utilising a solid fuel dual pulse rocket motor with a kolibri radio and laser proximity fuse with back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-20 m²

~400 km max range at 10 km+ altitude 

~300 km max Range at 5 km+ altitude 

~250 km max Range at sea level 

~200 km engagement range vs RCS of 1m² at sea level 

~250 km engagement range vs RCS of 1m² at 5 km+ altitude 

~300 km engagement range vs RCS of 1m² at 10 km+ altitude 

~90 km NEZ range vs RCS of 1m² at sea level 

~120 km NEZ range vs RCS of 1m² at 5 km> altitude

~150 km NEZ range vs RCS of 1m² at 10 km> altitude

~13 km ARH lock range vs RCS of 0.003m²

~40 km ARH lock range vs RCS of 1m²

~70 km ARH lock range vs RCS of 3m²

~90 km ARH lock range vs RCS of 10m²

~0.0005 m² minimum target RCS for ARH lock 

~8g launch limiter

~8g target limiter 

~40g overload tolerance 

~Targeting Angles 90°

~Turn Rate 10 to 60 Deg/s

~Initial Acceleration of 900-1200 m/s>

~Mach 6 max target velocity 

~Mach 6 top speed above 5 km altitude 

~Mach 4 top speed at sea level


R-37M

4+ Generation Radar Missile 

9B-1103M-350 Inverse Monopulse Ku/X band Active Seeker with an fully digital slotted planar antenna array with an INS/GNSS utilising a bi-directional radio correction data link with back up inertial operting guidance, home on jam, dual band seeker and polarisation filtering ECCM utilising a solid fuel dual pulse rocket motor with a laser and radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-20 m²

~400 km max range at 10 km+ altitude 

~300 km max Range at 5 km+ altitude 

~150 km max Range at sea level 

~120 km engagement range vs RCS of 3m² at sea level 

~200 km engagement range vs RCS of 3m² at 5 km+ altitude 

~300 km engagement range vs RCS of 3m² at 10 km+ altitude 

~70 km NEZ range vs RCS of 3m² at sea level 

~90 km NEZ range vs RCS of 3m² at 5 km> altitude

~120 km NEZ range vs RCS of 3m² at 10 km> altitude

~20 km ARH lock range vs RCS of 1m²

~40 km ARH lock range vs RCS of 3m²

~70 km ARH lock range vs RCS of 10m²

~0.005 m² minimum target RCS for ARH lock 

~Targeting Angles 45°

~Turn Rate 10 to 60 Deg/s

~Initial Acceleration of 600-900 m/s>

~8g launch limiter

~8g target limiter 

~40g overload tolerance 

~Mach 6 max target velocity 

~Mach 6 top speed above 5 km altitude 

~Mach 4 top speed at sea level


R-74M2

5th Generation IR Missile 

Karfagen-760 LN² Cooled MIR & UV channel fully digital pseudo-imaging HgCdTe LOAL Seeker with dual band, IOG, gatewidth and seeker shut off IRCCM

~50 km range at sea level 

~50 km engagement range 

~All aspect lock range 10 km

~Rear aspect lock range 10 km

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Flare rejection 0.9+

~Turn Rate 120 to 180 Deg/s

~Initial Acceleration of 300-400 m/s>

~Rectile Speed: 200 Hz

~Gimbal limit: 180°

~Angular Tracking: 75 deg/s 

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 80g 

Air to Ground Missiles  

3M22 5th Generation HE Cruise Missile 

Kh-69 LO 4th Gen Cluster Cruise Missile 

Kh-69 LO 4th Gen HEAT Cruise Missile 

Kh-59MK2-F-E LO 3rd Gen OG/IIR FRAG-HE 

Kh-59M2-M 2nd Generation OG HE 

Kh-59M2-K 2nd Generation OG HEAT 

Kh-59M2-KE 2nd Generation OG Cluster 

Kh-59M2D-M 2nd Generation OG/IIR HE 

Kh-59M2D-K 2nd Generation OG/IIR HEAT 

Kh-59M2D-KE 2nd Generation OG/IIR Cluster 

Kh-59MK-M 4th Generation HE Cruise Missile

Kh-59MK-K 4th Gen HEAT Cruise Missile

Kh-59MK-KE 4th Gen Cluster Cruise Missile

Kh-58UShKE 3rd Gen Anti Radiation  

Kh-58UShKE-TP 3rd Gen OG/IIR Anti Radiation

Kh-38ML-M 3rd Generation Laser Guided HE 

Kh-38ML-K 3rd Gen Laser Guided HEAT

Kh-38ML-KE 3rd Gen Laser Guided Cluster 

Kh-38MT-M 3rd Generation OG/IIR HE 

Kh-38MT-K 3rd Gen OG/IIR HEAT

Kh-38MT-KE 3rd Gen OG/IIR Cluster  

Kh-29MP-M 4th Gen HE Ballistic Missile 

Kh-29MP-K 4th Gen HEAT Ballistic Missile 

Kh-29TE-M 3rd Generation OG HE 

Kh-29TE-K 3rd Generation OG HEAT 

Kh-29TD-M 3rd Generation OG/IIR HE 

Kh-29TD-K 3rd Generation OG/IIR HEAT 

Kh-29ML-M 3rd Generation Laser Guided HE 

Kh-29ML-K 3rd Gen Laser Guided HEAT   


Laser Guided Bombs 

KAB-20LG-K 3rd Generation HEAT 

KAB-20LG-FE 3rd Generation FRAG-HE  

KAB-50LG-K 3rd Generation HEAT 

KAB-50LG-FE 3rd Generation FRAG-HE  

KAB-100LG-K 3rd Generation HEAT 

KAB-100LG-FE 3rd Generation FRAG-HE 

KAB-250LG 3rd Generation HE 

KAB-250LG-F-E 3rd Generation FRAG-HE 

KAB-250LG-OD-E 3rd Generation FAE

KAB-500MLG 3rd Generation HE

KAB-500MLG-Pr-E 3rd Gen Bunker Buster 

KAB-500MLG-F-E 3rd Generation FRAG-HE 

KAB-500MLG-OD-E 3rd Generation FAE 

KAB-500MLG-K-E 3rd Gen Cluster Bomb


Optically Guided Bombs 

KAB-50Kr-M-K 3rd Generation HEAT 

KAB-50Kr-MT-K 3rd Generation IIR HEAT 

KAB-50Kr-M-FE 3rd Generation FRAG-HE 

KAB-50Kr-MT-FE 3rd Generation IIR FRAG-HE 

KAB-100Kr-M-K 3rd Generation HEAT 

KAB-100Kr-MT-K 3rd Generation IIR HEAT 

KAB-100Kr-M-FE 3rd Generation FRAG-HE 

KAB-100Kr-MT-FE 3rd Gen IIR FRAG-HE

KAB-250Kr-M 3rd Generation HE 

KAB-250Kr-M-F-E 3rd Generation FRAG-HE 

KAB-250Kr-M-OD-E 3rd Generation FAE

KAB-500Kr-M 3rd Generation HE

KAB-500Kr-M-Pr-E 3rd Gen Bunker Buster 

KAB-500Kr-M-F-E 3rd Generation FRAG-HE 

KAB-500Kr-M-OD-E 3rd Generation FAE 

KAB-500Kr-M-K-E 3rd Gen Cluster Bomb


Bunker Busters 

Kh-59MKM 3rd Generation Bunker Buster 

Kh-59MK2-Pr LO 3rd Gen Bunker Buster 

KAB-500Kr-Pr-E 2nd Gen Bunker Buster 

KAB-500LG-Pr-E 2nd Gen Bunker Buster

KAB-250LG-Pr-E 2nd Generation Bunker Buster

BETAB-500SHP 1st Generation bunker buster

BETAB-500 1st Generation Bunker buster 

BETAB-500Y 1st Generation Bunker buster 


Satellite Guided Munitions 

Kh-25MS-M Satellite guided HE 

Kh-25MS-F Satellite guided FRAG-HE 

Kh-38MS-M Satellite guided HE 

Kh-38MS-F Satellite guided FRAG-HE 

KAB-20S-E satellite guided HE bomb 

KAB-50S-E Satellite guided HE bomb 

KAB-100S-E satellite guided HE bomb 

KAB-250S-E satellite guided HE bomb 

KAB-500S-E Satellite guided HE bomb 

KAB-500Kr UMPK Satellite guided TV bomb 

ZAB-100 UMPK satellite guided Incen bomb 

ZAB-250 UMPK satellite guided Incen bomb

ODAB-500 UMPK satellite guided FAE bomb 

RBK-500 UMPK satellite guided cluster bomb

FAB-250 UMPK satellite guided HE bomb 

FAB-500 UMPK satellite guided HE bomb 

FAB-250 UMPB satellite guided HE bomb 

FAB-500 UMPB satellite guided HE bomb 


Unguided Bombs 

FAB-250 Unguided HE Bomb 

FAB-500 Unguided HE Bomb 

OFAB-150 Unguided Frag Bomb 

OFAB-250 Unguided Frag Bomb 

OFAB-500 Unguided Frag Bomb 

PLAB-250-120 Unguided ASW bomb 

ZAB-100-105 Unguided Incendiary bomb

ZAB-250-200 Unguided Incendiary bomb 

ODAB-500 Unguided fuel air bomb 

PTAB-500 Unguided anti tank bomb 

PTAB-500Y Unguided Anti Tank bomb 


GSh-30-1 

30x165mm MKETF

30x165mm SAPHEI

30x165mm API-T

30x165mm HEI-T 


T-50 Prototypes 


Su-57 (pre production)


Su-57S

M model 




Su-35 Super Flanker Series 


Su-35 / Su-27M 

Prototype: 1988

Aircraft Role: Air Superiority  

Generation: 4+

Number made: 12+


Su-37

Prototype: 1996

Aircraft Role: Air Superiority 

Generation: 4+

Number made: 1


Su-35S 

Prototype: 2008

Completed: 2012

Production: 2014

Service: 2018

Aircraft Role: MultiRole / Air Superiority 

Generation: 4.5 

Combat Rank: S

Number Made: 200+


Su-35SM

Concept: 2022


Navigation: PrNK-27M fully computerised navigation suite with a SAU-10-11 6× axis computerised autopilot and an with a PNK-11 fully digital navigation system using Ts-061K 32x bit fully digital navigation computer using a fully digital INS utilising a ring laser gyroscope and gyrostabilized accelerometer with an accuracy of 0.04° in pitch and yaw and 0.07° in heading with an error rate of 1.3 km/ph and velocity error rate of <0.10 m/s with a hybridised position accuracy of <30m. RV-20 solid state radar altimeters. ARK-22 solid state ADF. RSDN-20 Alpha digital radio navigation system with DVOR and ILS with a position accuracy of 20-90m and angular accuracy of ±0.1°. SNS-85 GLONASS Global navigation satellite system with a max CEP of 5m and average CEP of 30m.


Flight Control: SUU-27 digital flight control system. SDU-10 analogue fly by wire AFCS utilising a Ts-080-1 16x bit digital ADC. ZSh-7 Flight Helmet. SOI-27 3rd Generation cockpit with 3× polychrome CRT MFDs with a HOTAS control stick. 


(37 adds PrNK-37 fully computerised navigation suite with a SAU-37 6× axis computerised autopilot and a SDU-37 fully digital fly by wire AFCS utilising a Ts-108 32x bit digital ADC with an TsPNK-11 fully digital navigation system utilising a Ts-061K 32x bit fully digital navigation computer using a fully digital INS utilising a ring laser gyroscope and gyrostabilized accelerometer with an accuracy of 0.04° in pitch and yaw and 0.07° in heading with an error rate of 1.3 km/ph.  RSBN-85 Vstrecha fully digital radio navigation system with DVOR and ILS with a position accuracy of 10-20m and angular accuracy of ±0.01°. MFD-11 4th Generation Cockpit with 3× HD LCD MFDs and a HOTAS control stick. ZSh-7AP Flight Helmet. A-737-10 GLONASS-M Global navigation satellite system with a max CEP of 2m and average CEP of 10m. (When inside former USSR airspace SDCM GNSS augmentation improves precision with a max CEP of 1m and average CEP of <4m) ARK-25 digital ADF. RV-21 digital radar altimeter. N011M-R fully digital navigation radar) 


(S model adds PrNK-35 fully computerised nav/attack suite with a SAU-35 6× axis computerised autopilot and a KSU-35 fully digital fly by wire AFCS utilising a 64x bit digital ADC with an IVS-35 all digital navigation system utilising a BINS-SP2 64x bit fully digital navigation computer using a fully digital combination INS with a digital tuning fork quartz, gimballed gyrostabilized accelerometer and ring laser gyroscope with an accuracy of 0.03° in pitch, yaw and heading with an error rate of <0.05 km/ph and velocity error rate of <0.3 m/s with a hybridised position accuracy of <5m. RSBN-85VM Vstrecha-M fully digital radio navigation system with DVOR and ILS with a position accuracy of <10m and angular accuracy of ±0.01°. MFD-35 5th Generation Cockpit with 3× UHD LCD MFDs and a HOTAS control stick. ZSh-7AP Flight Helmet. A-737-10 GLONASS-M Global navigation satellite system with a max CEP of 2m and average CEP of 10m. (When inside former USSR airspace SDCM GNSS augmentation improves precision with a max CEP of 1m and average CEP of <4m) ARK-35 fully digital ADF. RV-22 fully digital radar altimeter. N035 fully digital navigation radar) 


(2018 models onwards add PPA-S/V-KNS GLONASS-K Global navigation satellite system with a max CEP of 60cm and average CEP of 3m)


(SM model will add MFI-25 5th Generation cockpit with 1× UHD LCD MFD and HOTAS control stick. ZSh-10 Flight Helmet)


Fire Control: RLPU-27M computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with digital sensors with stability augmentation with RLPK-27 radar targeting and OEPS-27M electro optical, laser and infrared imaging/tracking targeting with the OEPrNK-10 data fusion system utilising NAV, IFF, RDR, IDL and IRST information displayed on one screen with a Ts-200 fully digital FCC utilising M1839 32x bit CPUs performing 50-75m IPS and 600-800m FLOPS. N011 Bars 4th Generation Radar with a digital X band mechanically steered monopulse system with a slotted planar antenna array using a data fused system with programmable digital signal processing, coherent doppler filtering and signal modulation based LDSD and pulse doppler IFF and tactical & missile data link integration with CW illumination for SARH guidance, low false alarm rates and computerised radar image displaying with multi-mode operation, radar map freezing, raid assessment, predictive flight path, non tracked target tracking, BIST system, air based JEM non cooperative target recognition functions and raster, conical, sector, circular and spiral scan scanning modes utilising GTD, GTT, TAR and TFR air to ground radar modes and SRC/LDSD, MR, STTR, MTTR and HMD, LDR, IRST, EOT and multi target RFR based ACMs air to air radar modes with gain modulation, notch filtering, low sidelobe antenna, polarization filtering and pulse compression ECCM with HPRF power output on average being 2 kW with a 10 kW max output with 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance and 1 channel for sidelobe suppression and ECM with a noise factor of 4 dB with a 960 mm antenna diameter. OLS-27K 2nd Generation IRST with a LN² cooled pseudoimaging InSb detector with an integrated 1.06 μm Nd:YAG laser rangefinder. ZSh-7 Flight Helmet with Shchel-3UM 1st Generation HMD utilising automatic cueing for targeting with head tracking software. IPV-1 4th Generation Radar display with an SVD system utilising a polychrome raster image displayed on a CRT MFD with computerised target generation, ECM resolution, navigation data and aircraft flight information with data link integration. 


(S model adds Sh-135 fully computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with fully digital sensors with full stability augmentation with an KPrNO-35 sensor fusion system utilising NAV, RDR, IRST, EOT, TDL, IFF, RHAWS, RFCM, IRCM, MAW, ESM and ECM information displayed on one screen with radar targeting fusion utilising the RLPK-35S radar targeting and the OEPS-35 electro optical, laser and infrared imaging/tracking targeting with a SOLO-35 all digital FCC utilising KOMDIV-64 64x bit 2× core CPUs performing 10-20b IPS and 150-200b FLOPS. N035 Irbis 5th Generation Radar utilising a mechanically and electronically steered fully digital X band Hybrid PESA system with a slotted planar antenna array using a sensor fused system with programmable fully digital signal processing, hybrid beam forming, coherent doppler filtering and signal modulation based LDSD with and pulse doppler IFF and tactical & missile data link integration with CW illumination for SARH guidance, very low false alarm rates, BIST system and fully computerised radar image displaying with simultaneous multi-mode operation, simultaneous searching tracking and guidance, radar map freezing, raid assessment, predictive flight path, non tracked target tracking, adaptive processing, automatic target recognition, multi target air and ground based SAR, JEM, RCS and HRRP non cooperative target recognition functions and agile beam, raster, palmer, conical, sector, circular and spiral scan scanning modes utilising DBS, I/SAR, RBGM, GTD, MGMTT, TAR, TFR, STI and MGMTI air to ground radar modes, FTT, I/SAR, SSD and SSTT air to sea modes and SRC/LDSD, MR, LPIR, ATC, STTR, MTTR and HMD, LDR, IRST, EOT and multi target RFR based ACMs air to air radar modes with gain modulation, notch filtering, sidelobe suppression, polarization filtering, tunable frequency filters, frequency hopping, home on jam, jammer identification and phase coded pulse compression ECCM with 1,840 R/Es broken up into 20 T/R modules utilising two EGSP-27 chelnok TWT transmitters and 4 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance, 1 channel for sidelobe suppression and ECM and 1 channel for FHSS scanning frequency with a noise factor of 4 dB with a 900 mm diameter antenna size and a HPRF power output on average being 5 kW with a 20 kW max output. 2× N036Sh Pokosnik 5th Generation electronically steered L band AESA radars with a quad radiator antenna array using a sensor fused system with programmable fully digital signal processing utilising low observability beacon interrogation and pulse doppler IFF integration with very low false alarm rates with a fully computerised radar image displayed with multi-mode operation, predictive flight path and non tracked target tracking functions and agile beam and spiral scan scanning modes utilising SRC, MTTR and STTR radar modes with sidelobe suppression, polarization filtering, frequency hopping and phase coded pulse compression ECCM with 48 GaAs T/R modules with a ~1100×100 mm antenna size with a HPRF power output on average being 8 kW with a 48 kW max output with 2 receiving channels with 1 channel for tracking and searching and 1 channel for ECM with a noise factor of 3 dB. IKSh-1M 5th Generation HUD with a fully digital LCD glass display utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with an integrated digital bombing complex utilising gun, bomb and rocket CCRP and CCIP with gun EEGS and a digital MFD with electro optical slaving, mission control, navigation systems and weapons functions. ZSh-7AP Flight Helmet with NSTsI-KOS 2nd Generation HMD utilising automatic cueing for targeting with navigation data and weapons management data displayed with head tracking. 5th Generation Radar display with an SVD system utilising a high resolution full colour raster image displayed on a LCD MFD with computerised target generation, ECM resolution, navigation data and aircraft flight information with data link integration. OLS-35 multi-channel fully digital EOTS with a HD resolution TV sight with a ~1080p day time image resolution, 1.06 μm Nd:YAG auto adjusting laser targeting system with laser rangefinding, laser designation and laser spot tracking and a 3rd Generation IRST & 3rd Generation FLIR system utilising a LN² cooled infrared imaging HgCdTe detector with an FPA format of 384x388 and a thermal image resolution of 776×768p. TsVB-54 fully digital ballistic computer utilising a KOMDIV-64 64x bit 2× core CPU enabling fully digitised automatic digital target lead and gun and missile coursing with gun, rocket and bomb CCRP and CCIP with a bomb and rocket accuracy of <3-5m CEP at a range up to 2000m and altitudes up to 5000m and <30-40m CEP at a range up to 10,000m and altitude up to 12,000m) 


(SM model will add fully computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with fully digital sensors with full stability augmentation with an IUS-35 sensor fusion system utilising the Sh-121 radar targeting and the OEPS-35 electro optical, laser and infrared imaging/tracking targeting with a SOLO-21 all digital FCC utilising Elbrus-8S 64x bit 8× core CPUs performing 30-40b IPS and 300-500b FLOPS. N036-1-01 5th Generation X band fully digital multimode AESA radar with a slotted planar array with 1629 GaAs T/R modules with a 900 mm antenna diameter with a HPRF power output on average being 10-12 kW with a 18 kW max output. ZSh-10B Helmet with NSTsI-50 3rd Generation HMD with integrated 4th Generation image intensifiers and 3rd Generation FLIR)


Communication & C2: K-DIAE digital unified communication complex with R-862/R-800 VHF/UHF and R-864 HF digital radios with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding and digital data encryption with text and voice formats utilised operating on 20 channels with data transfer speeds of 1.2 kbit/s, 10 kbit/s and 16 kbit/s with an operating communication range of 350 km with an integrated LChM FHSS system utilising up to 100 frequency hops per second and VChP CRNG encoding system with 10 round cryptographic encryption for 56 bit and 8 round cryptographic encryption for 96 bit and the TKS-2 digital information data link linked to the Voyska PVO NDCC air defence network with digital electronics, frequency hopping, ECM resistance, two way communication, digital data encryption, multi aircraft link, IFF integration, electronic countermeasure support and C2 integration utilising ground and air based computer and radar generated data exchange with pre recorded voice, text and image formats used, with data transfer speeds of 75 bit/s, 150 bit/s, 300 bit/s, 1200 bit/s, 2400 bit/s and 4800 bit/s every 2 to 10 seconds operating on 3 MHz to 300 MHz with up to 20,000 frequency hops per second on 26 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1000 km with data exchange between up to 16 aircraft. Rubezh-M digital GCI complex with the Spektr-1 and Biryusa digital navigation data links and BAN-75, SVPK, SPK-75 and SPK-68 digital command data links connected to the SAU-10-11 computerised autopilot, ARK-22 solid state ADF, SO-72 digital IFF interrogator and SRZO-2P solid state IFF transponder linked to the PVO NDCC air defence network with fully automated ground controlled interception, weapons management, IFF integration, digital data encryption and navigation data utilising ground based computer and radar generated data exchange with pre recorded voice and text formats used with data transfer speeds of 45 bit/s, 80 bit/s and 96 bit/s every 5 to 10 seconds operating on 2 MHz to 400 MHz with up to 1000 frequency hops per second on 10 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1000 km with data exchange between up to 36 aircraft. TsVM-90 fully digital FMC utilising MP1839L1 32x bit CPUs performing 25-50m IPS and 2-4b FLOPS with a 600-800k SLOC BTsK-10 RTOS with integrated aircraft health management software, digital navigation software, moving map display and data sharing. 


(37 model adds S-103 fully digital unified communication complex with an R-833 fully digital software defined VHF/UHF and HF radio with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding, rekeying encryption and full digital data encryption with text, image and voice formats utilised operating on 8 programmable channels and 256 frequency carriers with data transfer speeds of 16 kbit/s, 5 mbit/s and 11 mbit/s utilising an PPCh integrated FHSS and CRNG system utilising up to 1000 frequency hops per second and 7 round cryptographic encryption for 128 bit, 9 round cryptographic encryption for 192 bit and 10 round cryptographic encryption for 256 bit with an operating LOS communication range of 450 km and BLOS up to 5000 km with satellite link and the TCS-2M fully digital Tactical Data Link linked to NDMC NTsUO military command center utilising the YeESU-TZ military C4 network that organises coordination between the Voiska PVO-PRO air defence network and the PTK blue force tracking network with links to Andromeda-D, Akatsiya-E, Barnaul-T, Baikal-1ME, Universal-1E, Fundament-M and Polyana-D4M1 C2 softwares and Type-1B, Planet and VIP-117M3 data terminals with fully automated VOR, GCI and ILS with fully digital electronics, frequency hopping, ECM resistance, two way communication, navigation data, fully digital data encryption, multi aircraft link, multi platform subscription, weapons management, IFF integration, electronic countermeasure support and C4 integration utilising ground and air based computer and radar generated data exchange with pre recorded voice, text and image formats used, with data transfer speeds of 1024 bit/s, 1200 bit/s, 2.4 kbit/s, 4.8 kbit/s and 16 kbit/s every 1 to 2 seconds operating on 3 MHz to 300 MHz with up to 20,000 frequency hops per second on 26 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1500 km with data exchange between up to 20 subscribers. BTsVM-900 fully digital FMC utilising i486DX4-90 32x bit CPUs performing 2-3b IPS and 90-120b FLOPS utilising the RelMK32 1-2m SLOC RTOS using a BTsK-37 C2IS suite linked to the Voyska PVO NDCC air defence network with squads level blue force tracking, SATCOM integration, electronic countermeasure support, precision targeting, integrated aircraft health management software, digital navigation software, moving map display and data sharing) 


(S models add S-107-1 fully digital unified communication complex with an R-999 fully digital software defined VHF/UHF and HF radio with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding, rekeying encryption, amplitude and phase shift keying, pulse code modulation and full digital data encryption with text, video, image and voice formats utilised operating on 99 programmable channels and 512 frequency carriers with data transfer speeds of 16 kbit/s, 10 mbit/s and 30 mbit/s utilising an integrated PPCh-B FHSS and CRNG system utilising up to 20,000 frequency hops per second and 12 round cryptographic encryption for 128 bit, 14 round cryptographic encryption for 192 bit and 16 round cryptographic encryption for 256 bit with an operating LOS communication range of 450 km and BLOS unlimited with satellite link and the OSNOD fully digital tactical data link linked to the NDMC NTsUO military command center utilising the YeESU-TZ military C4 network that organises coordination between the Kavkaz-EASS military C3I radio communication network, Voiska PVO-PRO air defence network, ASUNO-S artillery network, PTK and Svod blue force tracking networks, Glaz-Groza UAV network and the Bylina electronic warfare network with links to BARS, Orbita, Andromeda-D, Strelets-M, Sagittarius-M, Akatsiya-E, Akatsiya-M, Barnaul-T, Baikal-1ME, Universal-1E, Fundament-M and Polyana-D4M1 C2 softwares and VIP-117M3, Lvin, 4RT-S, Legend, Planet, Type-1B, Kulon-V and Baget-K data terminals with two way communication, low observability data exchange, weapons management, radio communication integration, navigation data, IFF integration, SATCOM integration, fullly digital data encryption, ECM resistance, multi aircraft link, multi platform subscription, frequency hopping, electronic countermeasure support and C4 integration utilising ground, air and sea based computer, radar and electro optically generated data exchange with high resolution text, image, and pre recorded sound formats used with live video and voice formats displayed on tactical display, with data transfer speeds of 1024 bit/s, 2048 bit/s, 40 kbit/s, 100 kbit/s and 34.4 mbit/s every 0.5 to 1 seconds operating on 300 MHz to 3 GHz with up to 80,000 frequency hops per second on 60 frequency carriers enabling a LOS data transmission range up to 500 km and BLOS up to 1500 km and unlimited range with satellite link with data exchange between up to 1800 subscribers and unlimited with satellite link. Baget-53-31 fully digital FMC utilising KOMDIV-64SMP 64x bit 4× core CPUs performing 20-30b IPS and 200-300b FLOPS utilising the BagrOS-4000 4-5m SLOC RTOS using an IUS-35 C2ISR suite linked to the YeESU-TZ military C4 network with section to platoon level blue force tracking software, C4 integration, SATCOM integration, GNSS integration, electronic countermeasure support, surrounding land formation intelligence, digital navigation, moving map display, precision targeting, integrated aircraft health management software, reconnaissance software, data sharing and C2 software) 


(2018 models onwards use Baget-53-31M fully digital FMC utilising 1888TX018 64x bit 8× core CPUs performing 20-30b IPS and 300-400b FLOPS) 


(SM model will use S-111 fully digital low observability unified communication system with an KSS-50 fully digital radio with SATCOMS and an integrated FHSS system utilising up to 20,000 frequency hops per second. Baget-53-31M1 fully digital FMC utilising Elbrus-16S 64x bit 16× core CPUs performing 30-40b IPS and 400-600b FLOPS for FMC)


Targeting: Bars radar with a 180° horizontal scan range and ±90° vertical scan range enabling tracking of up to 12 targets and data linking of 4 missiles with with an Rmax range up to 400 km, 350 km detection range for 16m² and 150 km track range for an aircraft with an RCS of 5m² with a LDSD detection range of 120 km for 5m² and a LDSD track range of 80 km for an aircraft with an RCS of 5m² with a rangefinding radar gun engagement range up to 10 km with a 200 km ground detection range with a 60 km track range for tank sized targets with tracking of up to 4 ground targets with ground mapping up to 200 km, with base image resolutions of 100, 1000 and 3000 m at a spatial resolution size of 10, 100 and 200 km with radar imaging complete in 40 seconds with a tracking scan range of 120° in azimuth and ±30° in elevation and a scan time of 2 seconds with max tracking target velocity at over 4000 kph and stores tracking information for up to 10 non tracked target with predictive flight paths for non tracked targets up to 12 seconds with LDSD ground clutter rejection of 80> dB, NCTR for 1 target up to 30 km with a scan range of ±15° in azimuth and ±5° in elevation with up to 20 preprogrammed target identifiers and high chaff rejection with a MTBF of 100 to 200 hours. OLS-27K IRST with tracking of up to 2 targets and automatic target tracking with an angular resolution of 0.1° and max tracking rate of 120 deg/s enabling a max range up to 100 km with a 50 to 80 km detection range and 20 to 40 km rear track range with 15 km front track range for fighter sized targets and laser targeting system with laser rangefinding with an accuracy of 10m and a 8 km engagement range for aircraft with a horizontal FOV up to 120° and a vertical FOV of -15°/+60°. Shchel-3UM HMD with 120° horizontal FOV and ±30° vertical FOV up to 10 km.


(S models add Irbis radar with a 245° horizontal and ±120° vertical scan range enabling tracking of up to 30 targets and data linking of 8 missiles with a 400 km Rmax range, in 15-24° narrow beam mode detection range is 350 to 400 km vs RCS of 3m², 250 to 300 km vs RCS of 1m² and 80 to 100 km vs RCS of 0.01m², normal detection range of 400 km vs RCS of 5m² and track range of 200 km vs RCS of 3m² with a LDSD detection range of 250 km for 5m² and a LDSD track range of 200 km for an aircraft with an RCS of 3m² with a rangefinding radar gun engagement range up to 20 km with a max ground attack detection range up to 300 km and a track range for tank sized targets up to 90 km with tracking of 4 targets with ground mapping up to 300 km, with base image resolutions of 1, 3 and 10 m at a spatial resolution size of 100, 200 and 300 km with radar imaging complete in 30 seconds with a tracking scan range of 125° in azimuth and ±60° in elevation with a scan sweep in 0.2 seconds with max tracking target velocity at over 7408 kph and LPI target acquisition with over 300 frequency hops per second and a max LPI engagement range of 200 km vs RCS of 3m² and stores tracking information for up to 15 non tracked targets with predictive flight paths for non tracked targets up to 14 seconds with LDSD ground clutter rejection of 100> dB, NCTR for 2 targets up to 60> km with a scan range of ±30° in azimuth and ±15° in elevation with up to 120 preprogrammed target identifiers and high chaff rejection with a MTBF of 400 to 600 hours. N036Sh AESA radars have a 180° horizontal scan range with tracking of 30 targets and a 500 km Rmax range with a 400 km detection range for 3m² and 150 km track range for 0.1m². X/L band Radar Data fused targeting with a horizontal scan range of 245° and a ±120° vertical scan range enabling tracking of up to 30 targets and data linking of 8 missiles with an Rmax range up to 500 km, 400 km detection range for an aircraft with an RCS of 3m² and track range of 200 km for an aircraft with an RCS of 1m². OLS-35 fully stabilised sight with a fully digital electro optical system with a 1× optical magnification with an FOV of 75° and a 10× optical magnification with an FOV of 7.5° with an independent stabilised vertical movement of -15°/+60° and independent stabilised horizontal movement of 180° with a moving stabilisation accuracy of 0.1 mils in azimuth and elevation and minimum/maximum stabilised sight movements of 0.03/60 deg/s with an angular tracking rate of 60 deg/s with FLIR enabling a max range of 30 km, detection of tank sized targets up to 12 km and identification up to 3 km with detection of corvette sized warships up to 28 km with identification up to 20 km with detection of fighter sized targets up to 20 km and identification up to 4 km with an automatic target tracking range up to 8 km, TV sight enabling a max range of 20 km, detection of tank sized targets up to 13 km and identification up to 10 km with detection of fighter sized targets up to 16 km and identification up to 14 km with NFOV detection of corvette sized warships up to 18 km with identification up to 15 km, IRST with automatic target tracking, automatic target slaving and automatic target recognition with tracking of 4 targets with an Angular resolution of 0.05° and max tracking rate of 200 deg/s enabling a max range up to 180 km with a 120 to 150 km detection range and 70 to 90 km rear track range with 35 km front track range and a 60 km track range for ground targets and laser targeting with laser rangefinding, laser designation and laser spot tracking with an accuracy of 5m with a 20 km engagement range for aircraft and 30 km engagement range for ground targets. NSTsI-KOS HMD with a 170° horizontal FOV and -35°/+85° vertical FOV with a target engagement range up to 20 km) 


(SM model will add N036-1-01 X band nose AESA radar system)


Targeting Pods for S models 


T-220I 3rd Generation Targeting Pod with FHD EOTS with a ~1440p day time image resolution, Raduga-V 3rd Generation FLIR system utilising a 1PN136 matrix with a 388x384 FPA format, 776×768p thermal image resolution, 3-5 μm spectral range, pixel pitch of 15 μm, NETp of 30 mK and 50 Hz refresh rate with an integrated auto adjusting Nd:YAG laser targeting system with laser rangefinding, laser designation and laser spot tracking with an accuracy of 10m with utilising a fully digital telescopic electro optical sight with a day time 4× optical magnification with an FOV of 25°, 60× optical magnification with an FOV of 1.6° and a 120× electro optical magnification with an FOV of 0.8° with a night time 1× optical magnification with an FOV of 24°, 10× optical magnification with an FOV of 2.4° and a 20× optical magnification with an FOV of 1.2° with independent stabilised depth movement, an independent stabilised vertical movement of -170°/+10° and independent stabilised horizontal movement of 320° with a moving stabilisation accuracy of 0.05 in elevation and azimuth and minimum/ maximum stabilised sight movements of 0.01/60 deg/s with an angular tracking rate of 50 to 90 deg/s with tracking of up to 30 targets and locking of up to 8 with FLIR enabling a max range of 30 km, detection of tank sized targets up to 12 km and identification up to 3 km with detection of corvette sized warships up to 28 km with identification up to 20 km with detection of fighter sized targets up to 20 km and identification up to 4 km with automatic target tracking up to 8km , TV sight enabling a max range of 90 km, detection of tank sized targets up to 50 km and identification up to 45 km with detection of fighter sized targets up to 70 km and identification up to 60 km with detection of corvette sized warships up to 87 km with identification up to 80 km with a 40 km laser engagement range for ground targets. 



Airframes and Engines: CAD designed Composite construction with an RCS minimum of 10m². Crew of 1. Length 22 m. Height 5.7 m. Wingspan 14 m. Wing area 62 m². Frame weight 18,500 kg. Takeoff weight 34,000 kg. Max Fuel 11,500 kg. 2× Lyul'ka-Saturn AL-31-SM axial flow low bypass turbofans with a digital electronic engine control with 160 kN of thrust and 250 kN in afterburner. 


(S models add CAD composite construction LV Airframe with an RCS minimum of 1m². Crew of 1. Length 22 m. Height 5.9 m. Wingspan 15.3 m. Wing area 62 m². Frame weight 19,000 kg. Takeoff weight 38,500 kg. Max Fuel 11,500 kg. 2× Lyul'ka-Saturn AL-41-F1S 3D thrust vectoring variable bypass axial flow FADEC turbofans with supercruise with 172 kN of thrust and 284 kN in afterburner) 


Speed and Endurance: Top speed of mach 2.2 to 2.5 at 15 km+, mach 2 to 2.5 at 10 km+, mach 2 to 2.2 to at 5 km+ and mach 1 to 1.3 at sea level. Service Ceiling of 19 to 23 km. Combat Range of 1300-2000 km. Acceleration 7-13 seconds to mach 1 at sea level. Stall speed 110-160 kph. Take off distance is 600m with ATA payload to 1300m for full payload. Landing distance 900 to 1100m. In flight refueling. 


(S models add Top speed of mach 2.2 to 2.6 at 15 km+, mach 2.2 to 2.4 at 10 km+, mach 2 to 2.2 to at 5 km+ and mach 1 to 1.2 at sea level with supercruise at mach 1.1 at sea level and mach 1.4 at 10 km+. Service Ceiling of 19 to 23 km. Combat Range of 1300-2000 km. Acceleration 7-13 seconds to mach 1 at sea level. Stall speed 90-140 kph. Take off distance is 500m with ATA payload to 1200m for full payload. Landing distance 800 to 900m. In flight refueling) 


S models add 


Stealth: low visibility airframe, leading edge trail treating and heavy RAM coatings applied to engines, front, top and sides with radar blockers. Low visibility IFF. 

 

Airframe RCS 

RCS Minimum: 1m²

RCS Median: 2m²

RCS Average: 4-8m²


Manuvarabilities: Thrust to weight ratio of 1.1 at full air to air payload and 1.5 at half fuel/loadout and 0.9 at full loadout. Roll rate of 160 deg/s at high speed and 230 deg/s at low speed. Climb rate of 280-320 m/s. No AOA limit at low speeds with 59° angle of attack at mach 1>. 12 to 26 kph/s speed bleed at high g instantaneous maneuvers and 15 to 31 kph/s speed bleed at high g sustained maneuvers. Sustained G tolerance of 9g with an Overload Tolerance of 12g and wing break at 18g. Wing loading of 370-420 kg/m. 4× LERXs with pitch of ±40° and 2× canards with pitch of ±30°and 2× elevators with pitch of -40°.  


(S models add 3D thrust vectoring with ±15° in roll/yaw and ±8° in pitch with deflection at 60 deg/s. Thrust to weight ratio of 1.2 at full air to air payload and 1.5 at half fuel/loadout and 1 at full loadout. Roll rate of 200 deg/s at high speed and 280 deg/s at low speed. Climb rate of 280-320 m/s. No AOA limit at any speed. 7 to 16 kph/s speed bleed at high g instantaneous maneuvers and 5 to 19 kph/s speed bleed at high g sustained maneuvers. Sustained G tolerance of 10g with an Overload Tolerance of 13g and wing break at 19.5-26g. Wing loading of 370-410 kg/m. 4× LERXs with pitch of ±90° and 2× elevators with pitch of -60°)


(SM model will add AL-51-F1S turbofans with 2D thrust vectoring with ±30° in yaw/roll with deflection at 60 deg/s)


Aircraft Turn Rates 


Sustained turn rates 


Mach ~1.5 Speeds 

● 1-2 deg/s at 10 km altitude 

● 3-5 deg/s at 5 km altitude 

● 5-8 deg/s at sea level  


Mach ~1 Speeds 

● 9-10 deg/s at 10 km altitude 

● 12-14 deg/s at 5 km altitude 

● 15-18 deg/s at sea level  


Mach 0.5> Speeds 

● 14-16 deg/s at 10 km altitude 

● 16-19 deg/s at 5 km altitude 

● 20-24 deg/s at sea level  


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 4-5 deg/s at 10 km altitude 

● 6-8 deg/s at 5 km altitude 

● 7-10 deg/s at sea level  


Mach ~1 Speeds 

● 15-17 deg/s at 10 km altitude 

● 17-20 deg/s at 5 km altitude 

● 19-23 deg/s at sea level  


Mach 0.5> Speeds 

● 24-27 deg/s at 10 km altitude 

● 27-31 deg/s at 5 km altitude 

● 29-34 deg/s at sea level  


S model adds


Sustained turn rates 


Mach ~1.5 Speeds 

● 5-6 deg/s at 10 km altitude 

● 8-10 deg/s at 5 km altitude 

● 11-14 deg/s at sea level  


Mach ~1 Speeds 

● 12-13 deg/s at 10 km altitude 

● 16-18 deg/s at 5 km altitude 

● 19-22 deg/s at sea level  


Mach 0.5> Speeds 

● 22-24 deg/s at 10 km altitude 

● 25-28 deg/s at 5 km altitude 

● 28-32 deg/s at sea level  


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 9-10 deg/s at 10 km altitude 

● 13-15 deg/s at 5 km altitude 

● 17-20 deg/s at sea level  


Mach ~1 Speeds 

● 18-20 deg/s at 10 km altitude 

● 22-25 deg/s at 5 km altitude 

● 27-31 deg/s at sea level  


Mach 0.5> Speeds 

● 27-30 deg/s at 10 km altitude 

● 34-38 deg/s at 5 km altitude 

● 40-45 deg/s at sea level 


Counter Measures: L-150/SPO-32 Pastel 3rd Generation fully digital RHAWS with 16 targets tracked and 128> preprogrammed threat identifiers with guidance of up to 6 ARMs with 2 fired simultaneous and 10× receivers enabling a self protection envelope of 360° in azimuth and ±60° in elevation with band coverage of 1.2-18 GHz with a signal detectability range up to 320 km.. SSP-2I digital fire countermeasure system. K-36DM Zero-Zero ejection seat. APP-50 countermeasure dispenser utilising 1st Generation IRCM and RFCM with 192 total rounds using the PPR-50 composite aluminium chaff that activates in 0.3 seconds and creates a false target RCS of greater than 60m² and using the PPI-50 thermite based flare with a minimum burn time of 3 seconds. SO-72/SRZO-2P 2nd Generation digital IFF interrogator / transponder linked to the Parol-2D fully digital IFF system with aircraft ID, full digital data encryption, radio/inertial navigation locating, reprogramming and cryptographic encoding. P-591 digital ICAS. KKO-15LP digital full ECLSS. 


(35S models add L-150-35/SPO-32M Pastel-M 4th Generation fully digital data fused RHAWS with 20 targets tracked with 242> preprogrammed threat identifiers with guidance of up to 8 ARMs with 4 fired simultaneous with 16× receivers enabling a self protection envelope of 360° in azimuth and elevation with band coverage of 0.2-20 GHz with a signal detectability range up to 440 km. 6× SOAR IR MAW receivers covering a spectral range of 3 to 5 µm enabling a protection envelope of 360° in azimuth and ±180° in elevation with a launch detection range of 70 km> and course trajectory detection range of <9 km. 4× SOLO laser warning receivers covering a pulse repetition frequency of 0.1 to 70 Hz and pulse duration of 60 ks and spectral range of 0.9 to 1.7 µm enabling a protection envelope of 360° in azimuth and ±90° in elevation. UV-50 countermeasure dispensers utilising 2nd Generation IRCM and 3rd Generation RFCM with 84 total rounds using PPR-50-17-110V composite aluminium jammer assisted chaff that activates in 0.3 seconds and creates a false target RCS greater than 60m², PPI-50-3 spectral flare with a minimum burn time of 3 seconds and Lobushka disposable DRFM jammers with a jamming time up to 6 seconds. Blesna Diamant-S 3rd Generation RFCM with a towed decoy SPJ with a 100m towing range utilising simultaneous LPIR, monopulse, continuous wave and pulse doppler countermeasure. Type 4283MP/Type 4280MD fully digital low observability IFF interrogator / transponder linked to the Parol-2D fully digital IFF system with aircraft ID, full digital data encryption, radio/inertial navigation locating, reprogramming and cryptographic encoding. SOZhE fully digital ICAS, full ECLSS and fire countermeasure system. K-36D-5 Zero-Zero ejection seat) 


(From early 2020s onwards Parol-2D is replaced by Password-3 all digital IFF system with aircraft ID, low observability data sharing, satellite navigation locating, full digital data encryption, reprogramming and cryptographic encoding)


Electronic Warfare: L-005S Sorbitsya-S 3rd Generation digital SPJ with monopulse countermeasure, continuous wave countermeasure and pulse doppler countermeasure ECCM with track breaker, track breaking and blip enhancement ELINT with 4× receivers enabling an ECCM protection envelope of 360° in azimuth with a self protection jamming range of 200 km> with SPS-171 3rd Generation digital active jamming system operating on 6-10 GHz with deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, cross eye jamming and spot jamming jamming ECM with 4× PESA pyramidal horn antenna ECM transmitters enabling an active jamming range of 200 km>. 


(Early 35S model adds L-175U Khibiny-U 4th Generation fully digital SPJ utilising radio direction finder with AoA and PRF determination, simultaneous monopulse countermeasure, continuous wave countermeasure, pulse doppler countermeasure and LPIR countermeasure with doppler shifting, home on jam and anti burn though ECCM with track breaker, advanced decoy generation, blip enhancement and global navigation spoofing ELINT with 6× receivers enabling a passive ECCM protection envelope of 360° in azimuth with a self protection jamming range of 300 km> with SAP-518 4th Generation fully digital active jamming system operating on 5-18 GHz with frequency agile deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, cross eye jamming, spot jamming, wave jamming, power managed jamming and DRFM jamming ECM with 4× GaAs AESA pyramidal horn antenna ECM transmitters enabling an active jamming range of 300 km>) 


(2018 35S models add L-265M10-35 Khibiny-M 5th Generation fully digital ECM System with an SPJ suite utilising radio direction finder with AoA and PRF determination, simultaneous monopulse countermeasure, continuous wave countermeasure, pulse doppler countermeasure and LPIR countermeasure with doppler shifting, noise cloaking, home on jam, anti burn though and self jam resistance ECCM with track breaker, advanced decoy generation, blip enhancement, satellite interception and global navigation spoofing ELINT with 8× receivers enabling a passive ECCM protection envelope of 360° in azimuth with a self protection jamming range of 400 km> with SAP-518SM 5th Generation fully digital active jamming system operating on 2-20 GHz with frequency agile deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, interrupted jamming, cross eye jamming, spot jamming, wave jamming, power managed jamming and DRFM/ISRJ jamming ECM with 4× GaN AESA pyramidal horn antenna array ECM transmitters enabling an active jamming range of 400 km>)


Guns: GSh-30-1 30mm autocannon slaved to HMD, laser rangefinder, IRST and radar with an effective firing range up to 2 km. 


Ordinance Capacity: 12× hardpoints with a max 7000 kg munition capacity and 150 rounds for the gun. 


(S models add 12× hardpoints with a max 10,000 kg munition capacity with 150 rounds for the gun)


Common Air to Air Payloads 

● 6× AKU-170 racks with R-77 2× APU-73 racks with R-74 2× SAP-518 

● 4× APU-470 racks with R-27ER 4× AKU-170 racks with R-77 2× APU-73 racks with R-74


R-77

4th Generation Radar Missile 

9P-1348 Inverse Monopulse X band Active Seeker with a slotted planar antenna array with an INS utilising a radio correction data link with back up inertial operting guidance, home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a Z23nA radio proximity fuse and back up impact detonation with with a high explosive blast warhead enabling a blast radius of 10-15 m²

~150 km max Range at 10 km+ altitude 

~120 km max Range at 5 km+ altitude 

~58 km max Range at sea level 

~35 km engagement range vs RCS of 5m² at sea level 

~80 km engagement range vs RCS of 5m² at 5 km+ altitude 

~110 km engagement range vs RCS of 5m² at 10 km+ altitude 

~15 km NEZ range vs RCS of 5m² at sea level 

~25 km NEZ range vs RCS of 5m² at 5 km> altitude

~30 km NEZ range vs RCS of 5m² at 10 km> altitude

~6 km ARH lock range vs RCS of 1m²

~18 km ARH lock range vs RCS of 5m²

~24 km ARH lock range vs RCS of 10m²

~0.1 m² minimum target RCS for ARH lock 

~Mach 5 max target velocity 

~Mach 4 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~50g Overload Tolerance 

~8g launch limiter

~10g target limiter 


R-27ER

3rd Generation Radar Missile 

9B-1101E Inverse Monopulse X band Semi Active Seeker with a phase comparison antenna array with an INS utilising a radio correction data link with back up inertial operting guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a radio proximity fuse and back up impact detonation with a continuous rod warhead enabling a blast radius of 10-15 m²

~130 km max Range at 10 km+ altitude 

~110 km max Range at 5 km+ altitude 

~90 km max Range at sea level 

~70 km engagement range vs RCS of 5m² at sea level 

~90 km engagement range vs RCS of 5m² at 5 km+ altitude 

~110 km engagement range vs RCS of 5m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 5m² at sea level 

~30 km NEZ range vs RCS of 5m² at 5 km> altitude

~50 km NEZ range vs RCS of 5m² at 10 km> altitude

~Mach 5 max target velocity 

~Mach 5 top speed above 5 km altitude 

~Mach 3 top speed at sea level

~Targeting Angles 35°

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~60g Overload Tolerance 

~8g launch limiter 

~10g target limiter 



R-27ET 

3rd Generation IR Missile 

Geofizika-36TE LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~120 km max Range at altitude 

~40 km max Range at sea level 

~80 km engagement range 

~All aspect lock range 20 km

~Rear aspect lock range 30 km

~Mach 4 at high altitude 

~Mach 2.5 at sea level 

~Rectile Speed: 125 Hz

~Flare rejection 0.6

~Gimbal limit: 55°

~Angular Tracking: 60 deg/s 

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 60g 



R-74

4th Generation IR Missile 

Mayak-80B LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~30 km max Range at 5 km> altitude 

~20 km max Range at sea level 

~20 km engagement range at 5 km>

~All aspect lock range 6 km

~Rear aspect lock range 10 km

~Mach 3 at 5 km> altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.6

~Gimbal limit: 60°

~Angular Tracking: 60 deg/s 

~Turn Rate 90 to 120 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 60g 


37 model adds 


R-77-1A

4th Generation Radar Missile 

9B-1248 Inverse Monopulse X band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a bi-directional radio correction data link with back up inertial operting guidance, home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser and Z23nA radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~150 km max Range at 10 km+ altitude 

~120 km max Range at 5 km+ altitude 

~90 km max Range at sea level 

~50 km engagement range vs RCS of 5m² at sea level 

~90 km engagement range vs RCS of 5m² at 5 km+ altitude 

~120 km engagement range vs RCS of 5m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 5m² at sea level 

~30 km NEZ range vs RCS of 5m² at 5 km> altitude

~40 km NEZ range vs RCS of 5m² at 10 km> altitude

~6 km ARH lock range vs RCS of 1m²

~18 km ARH lock range vs RCS of 5m²

~24 km ARH lock range vs RCS of 10m²

~0.1 m² minimum target RCS for ARH lock 

~Mach 5 max target velocity 

~Mach 4 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~Launch limiter 9g 

~Target limiter 10g 

~Overload Tolerance 50g



S models add 


Common Air to Air Payloads 

● 4× AKU-170M dual racks with R-77-1 6× AKU-170 racks with R-77-1 2× APU-73 racks with R-74M 

● 4× AKU-170M dual racks with R-77-1 4× AKU-170 racks with R-77-1 2× APU-73 racks with R-74M 2× SAP-518SM wing pods 

● 5× AKU-620 racks with R-37M 5× AKU-170 racks with R-77-1 2× APU-73 racks with R-74M 

● 4× AKU-620 racks with R-37M 4× AKU-170 racks with R-77-1 2× APU-73 with R-74M 2× SAP-518SM wing pods



R-77-1B

4+ Generation Radar Missile 

9B-1103M-150 Inverse Monopulse X/Ku band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a bi-directional radio correction data link with back up inertial operting guidance, dual band, home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser and Z23nA radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~200 km max Range at 10 km+ altitude 

~150 km max Range at 5 km+ altitude 

~80 km max Range at sea level 

~50 km engagement range vs RCS of 5m² at sea level 

~110 km engagement range vs RCS of 5m² at 5 km+ altitude 

~140 km engagement range vs RCS of 5m² at 10 km+ altitude 

~30 km NEZ range vs RCS of 5m² at sea level 

~40 km NEZ range vs RCS of 5m² at 5 km> altitude

~60 km NEZ range vs RCS of 5m² at 10 km> altitude

~8 km ARH lock range vs RCS of 1m²

~20 km ARH lock range vs RCS of 5m²

~26 km ARH lock range vs RCS of 10m²

~0.05 m² minimum target RCS for ARH lock 

~Mach 5 max target velocity 

~Mach 4 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~Launch limiter 9g 

~Target limiter 10g 

~Overload Tolerance 50g



R-37M

4+ Generation Radar Missile 

9B-1103M-350 Inverse Monopulse Ku/X band Active Seeker with an fully digital slotted planar antenna array with an INS/GNSS utilising a bi-directional radio correction data link with back up inertial operting guidance, home on jam, dual band seeker and polarisation filtering ECCM utilising a solid fuel dual pulse rocket motor with a laser and radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-20 m²

~400 km max range at 10 km+ altitude 

~300 km max Range at 5 km+ altitude 

~150 km max Range at sea level 

~120 km engagement range vs RCS of 3m² at sea level 

~200 km engagement range vs RCS of 3m² at 5 km+ altitude 

~300 km engagement range vs RCS of 3m² at 10 km+ altitude 

~70 km NEZ range vs RCS of 3m² at sea level 

~90 km NEZ range vs RCS of 3m² at 5 km> altitude

~120 km NEZ range vs RCS of 3m² at 10 km> altitude

~20 km ARH lock range vs RCS of 1m²

~40 km ARH lock range vs RCS of 3m²

~70 km ARH lock range vs RCS of 10m²

~0.005 m² minimum target RCS for ARH lock 

~Targeting Angles 45°

~Turn Rate 10 to 60 Deg/s

~Initial Acceleration of 600-900 m/s>

~8g launch limiter

~8g target limiter 

~40g overload tolerance 

~Mach 6 max target velocity 

~Mach 6 top speed above 5 km altitude 

~Mach 4 top speed at sea level


R-27ET 

4th Generation IR Missile 

Geofizika-36TE LN² Cooled digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~120 km max Range at altitude 

~40 km max Range at sea level 

~80 km engagement range 

~All aspect lock range 20 km

~Rear aspect lock range 30 km

~Angular tracking 60 deg/s

~Mach 4 at high altitude 

~Mach 2.5 at sea level 

~Rectile Speed: 125 Hz

~Flare rejection 0.6

~Gimbal limit: 55°

~Angular Tracking: 60 deg/s 

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 60g 


R-74M

4+ Generation IR Missile 

Impuls-90 LN² Cooled NIR & UV channel fully digital pseudo-imaging HgCdTe Seeker with dual band, gatewidth and seeker shut off IRCCM

~50 km max Range at 5 km> altitude 

~40 km max Range at sea level 

~40 km engagement range at 5 km> altitude

~All aspect lock range 10 km

~Rear aspect lock range 10 km 

~Mach 3 at 5 km> altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.8

~Gimbal limit: 75°

~Angular Tracking: 60 deg/s 

~Turn Rate 120 to 180 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 80g 



Air to Air Missiles 

R-77-1 3rd Generation Radar Missile 

R-37M 3rd Generation Radar Missile 

R-27EA 3rd Generation Radar Missile 

R-74M 3rd Generation IR Missile 


Air to Ground Missiles  

Kh-69 LO 4th Gen Cluster Cruise Missile 

Kh-69 LO 4th Gen HEAT Cruise Missile 

Kh-59MK2-F-E LO 3rd Gen OG/IIR FRAG-HE 

Kh-59M2-M 2nd Generation OG HE 

Kh-59M2-K 2nd Generation OG HEAT 

Kh-59M2-KE 2nd Generation OG Cluster 

Kh-59M2D-M 2nd Generation OG/IIR HE 

Kh-59M2D-K 2nd Generation OG/IIR HEAT 

Kh-59M2D-KE 2nd Generation OG/IIR Cluster 

Kh-59MK-M 4th Generation HE Cruise Missile

Kh-59MK-K 4th Gen HEAT Cruise Missile

Kh-59MK-KE 4th Gen Cluster Cruise Missile

Kh-58UShKE 3rd Gen Anti Radiation  

Kh-58UShKE-TP 3rd GenOG/IIR Anti Radiation

Kh-29MP-M 4th Gen HE Ballistic Missile 

Kh-29MP-K 4th Gen HEAT Ballistic Missile 

Kh-29TE-M 3rd Generation OG HE 

Kh-29TE-K 3rd Generation OG HEAT 

Kh-29TD-M 3rd Generation OG/IIR HE 

Kh-29TD-K 3rd Generation OG/IIR HEAT 

Kh-29ML-M 3rd Generation Laser Guided HE 

Kh-29ML-K 3rd Gen Laser Guided HEAT   


Laser Guided Bombs 

KAB-20LG-K 3rd Generation HEAT 

KAB-20LG-FE 3rd Generation FRAG-HE  

KAB-50LG-K 3rd Generation HEAT 

KAB-50LG-FE 3rd Generation FRAG-HE  

KAB-100LG-K 3rd Generation HEAT 

KAB-100LG-FE 3rd Generation FRAG-HE 

KAB-250LG 3rd Generation HE 

KAB-250LG-F-E 3rd Generation FRAG-HE 

KAB-250LG-OD-E 3rd Generation FAE

KAB-500MLG 3rd Generation HE

KAB-500MLG-Pr-E 3rd Gen Bunker Buster 

KAB-500MLG-F-E 3rd Generation FRAG-HE 

KAB-500MLG-OD-E 3rd Generation FAE 

KAB-500MLG-K-E 3rd Gen Cluster Bomb


Optically Guided Bombs 

KAB-20Kr-MT-FE 3rd Generation IIR FRAG-HE 

KAB-50Kr-M-K 3rd Generation HEAT 

KAB-50Kr-MT-K 3rd Generation IIR HEAT 

KAB-50Kr-M-FE 3rd Generation FRAG-HE 

KAB-50Kr-MT-FE 3rd Generation IIR FRAG-HE 

KAB-100Kr-M-K 3rd Generation HEAT 

KAB-100Kr-MT-K 3rd Generation IIR HEAT 

KAB-100Kr-M-FE 3rd Generation FRAG-HE 

KAB-100Kr-MT-FE 3rd Gen IIR FRAG-HE

KAB-250Kr-M 3rd Generation HE 

KAB-250Kr-M-F-E 3rd Generation FRAG-HE 

KAB-250Kr-M-OD-E 3rd Generation FAE

KAB-500Kr-M 3rd Generation HE

KAB-500Kr-M-Pr-E 3rd Gen Bunker Buster 

KAB-500Kr-M-F-E 3rd Generation FRAG-HE 

KAB-500Kr-M-OD-E 3rd Generation FAE 

KAB-500Kr-M-K-E 3rd Gen Cluster Bomb


Bunker Busters 

Kh-59MKM 3rd Generation Bunker Buster 

Kh-59MK2-Pr LO 3rd Gen Bunker Buster 

KAB-500Kr-Pr-E 2nd Gen Bunker Buster 

KAB-500LG-Pr-E 2nd Gen Bunker Buster

KAB-250LG-Pr-E 2nd Generation Bunker Buster

BETAB-500SHP 1st Generation bunker buster

BETAB-500 1st Generation Bunker buster 

BETAB-500Y 1st Generation Bunker buster 


Satellite Guided Munitions 

Kh-25MS-M Satellite guided HE 

Kh-25MS-F Satellite guided FRAG-HE 

Kh-38MS-M Satellite guided HE 

Kh-38MS-F Satellite guided FRAG-HE 

KAB-20S-E satellite guided HE bomb 

KAB-50S-E Satellite guided HE bomb 

KAB-100S-E satellite guided HE bomb 

KAB-250S-E satellite guided HE bomb 

KAB-500S-E Satellite guided HE bomb 

KAB-500Kr UMPK Satellite guided TV bomb 

ZAB-100 UMPK satellite guided Incen bomb 

ZAB-250 UMPK satellite guided Incen bomb

ODAB-500 UMPK satellite guided FAE bomb 

RBK-500 UMPK satellite guided cluster bomb

FAB-250 UMPK satellite guided HE bomb 

FAB-500 UMPK satellite guided HE bomb 

FAB-250 UMPB satellite guided HE bomb 

FAB-500 UMPB satellite guided HE bomb 


Unguided Bombs 

FAB-250 Unguided HE Bomb 

FAB-500 Unguided HE Bomb 

OFAB-150 Unguided Frag Bomb 

OFAB-250 Unguided Frag Bomb 

OFAB-500 Unguided Frag Bomb 

PLAB-250-120 Unguided ASW bomb 

ZAB-100-105 Unguided Incendiary bomb

ZAB-250-200 Unguided Incendiary bomb 

ODAB-500 Unguided fuel air bomb 

PTAB-500 Unguided anti tank bomb 

PTAB-500Y Unguided Anti Tank bomb 


Rockets 

S-25L 2nd Generation laser guided rocket

S-25-OFM 1st Generation Bunker buster 

S-25-OF high explosive Rocket 

S-13B 1st Generation Bunker buster 

S-13T tandem HEAT AT round 

S-13OF AP Anti armour frag round 

S-13DF thermobaric round 

S-13Kor 2nd Generation laser guided rocket


GSh-30-1 

30x165mm MKETF

30x165mm SAPHEI

30x165mm API-T

30x165mm HEI-T 


Later models would add (SM will also use)


● 4× AKU-170M dual racks with R-77M 4× AKU-170 racks with R-77M 2× APU-73 racks with R-74M2 2× SAP-518SM wing pods

● 4× AKU-170M dual racks with R-77M 6× AKU-170 racks with R-77M 2× APU-73 racks with R-74M2


R-77-1C

4+ Generation Radar Missile 

9B-1103M-200PA Inverse Monopulse Ku band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a bi-directional radio correction data link with back up inertial operting guidance, home on jam, multimode guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser and Z23nA radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~200 km max Range at 10 km+ altitude 

~150 km max Range at 5 km+ altitude 

~80 km max Range at sea level 

~50 km engagement range vs RCS of 3m² at sea level 

~100 km engagement range vs RCS of 3m² at 5 km+ altitude 

~120 km engagement range vs RCS of 3m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 3m² at sea level 

~40 km NEZ range vs RCS of 3m² at 5 km> altitude

~60 km NEZ range vs RCS of 3m² at 10 km> altitude

~10 km ARH lock range vs RCS of 1m²

~20 km ARH lock range vs RCS of 3m²

~30 km ARH lock range vs RCS of 10m²

~0.05 m² minimum target RCS for ARH lock 

~Mach 5 max target velocity 

~Mach 4 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~Launch limiter 9g 

~Target limiter 12g 

~Overload Tolerance 60g


R-77M

5th Generation Radar Missile 

9B-1103M2 Ka/Ku band AESA Active Seeker with 64 GaAs T/R modules using an fully digital patch antenna array with an INS/GNSS utilising a bi-directional radio correction data link with back up inertial operting guidance, LPIR, home on jam, dual band seeker and polarisation filtering ECCM utilising a solid fuel dual pulse rocket motor with a laser and radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~300 km max Range at 10 km+ 

~250 km max Range at 5 km+

~150 km max Range at sea level 

~120 km engagement range vs RCS of 1m² at sea level 

~190 km engagement range vs RCS of 1m² at 5 km+ altitude 

~220 km engagement range vs RCS of 1m² at 10 km+ altitude 

~50 km NEZ range vs RCS of 1m² at sea level 

~70 km NEZ range vs RCS of 1m² at 5 km> altitude

~90 km NEZ range vs RCS of 1m² at 10 km> altitude

~2 km ARH lock range vs RCS of 0.003m²

~14 km ARH lock range vs RCS of 1m²

~26 km ARH lock range vs RCS of 3m²

~35 km ARH lock range vs RCS of 10m²

~0.0005 m² minimum target RCS for ARH lock 

~Mach 6 max target velocity 

~Mach 5 top speed above 5 km altitude 

~Mach 3 top speed at sea level

~Targeting Angles 60°

~Turn Rate 70 to 120 Deg/s

~Initial Acceleration of 300-600 m/s>

~Launch limiter 10g 

~Target limiter 12g 

~Overload Tolerance 80g


R-74M2

5th Generation IR Missile 

Karfagen-760 LN² Cooled MIR & UV channel fully digital pseudo-imaging HgCdTe LOAL Seeker with dual band, IOG, gatewidth and seeker shut off IRCCM

~60 km max Range 

~50 km range at sea level 

~50 km engagement range 

~All aspect lock range 10 km

~Rear aspect lock range 10 km

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Flare rejection 0.9+

~Turn Rate 120 to 180 Deg/s

~Initial Acceleration of 300-400 m/s>

~Rectile Speed: 200 Hz

~Gimbal limit: 180°

~Angular Tracking: 75 deg/s 

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 80g 



Su-35 


Su-37 


Su-35S 


Su-35SM





Su-34 Fullback Series


Su-32 / Su-27IB 

Designed: 1989

Prototype: 1990

Generation: 4+

Aircraft Role: MultiRole/Strike Fighter 

Combat Rank: D

Number Made: 8


Su-34

Prototype: 1993

Completed: 1994

Production: 1995

Service: 2004

Generation: 4+

Aircraft Role: MultiRole/Strike Fighter 

Combat Rank: S

Number Made: 200+


Su-34M

Prototype: 2018

Completed: 2021

Production: 2023

Service: 2024

Generation: 4.5 

Aircraft Role: MultiRole/Strike Fighter 

Combat Rank: S

Number Made: 80+


Engine and Airframe: CAD designed Composite construction with an RCS minimum of 5m². Crew of 2. Length 23.3 m. Height 6.1 m. Wingspan 14.7 m. Wing area 62 m². Frame weight 22,500 kg. Takeoff weight 45,100 kg. Max Fuel 12,100 kg 2× Lyul'ka-Saturn AL-31-SM axial flow low bypass turbofans with a digital electronic engine control with 160 kN of thrust and 255 kN in afterburner.  Refueling boom. 


(34 adds  2× Lyul'ka-Saturn AL-31FM2 axial flow low bypass turbofans with a digital electronic engine control with 160 kN of thrust and 264 kN in afterburner) 


Speed and Endurance: Top speed of mach 2 to 2.2 at 15 km+, mach 1.8 to 2 at 10 km+, mach 1.6 to 1.8 to at 5 km+ and mach 1 to 1.1 at sea level. Service Ceiling of 17 to 23 km. Combat Range of 800-1200 km. Acceleration 13-22 seconds to mach 1 at sea level. Stall speed 240-330 kph. Take off distance is 700m with ATA payload to 1200m for full payload. Landing distance 700 to 900m. In flight refueling. 


(M model adds 2× Lyul'ka-Saturn AL-41-F1S 3D thrust vectoring variable bypass axial flow FADEC turbofans with supercruise with 168 kN of thrust and 275 kN in afterburner with a Top speed of mach 2 to 2.4 at 15 km+, mach 2 to 2.2 at 10 km+, mach 1.8 to 2 to at 5 km+ and mach 1 to 1.2 at sea level with supercruise at mach 1 at sea level and mach 1.2 at 10 km+. Service Ceiling of 17 to 23 km) 


Manuvarabilities: Thrust to weight ratio of 0.9 at full air to air payload and 1 at half fuel/loadout and 0.7 at full loadout. Roll rate of 180 deg/s at high speed and 200 deg/s at low speed. Climb rate of 170-220 m/s. Angle of Attack at 28° at mach 1> and 47° at mach <1. 23 to 56 kph/s speed bleed at high g instantaneous maneuvers and 15 to 58 kph/s speed bleed at high g sustained maneuvers. Wing loading of 450-520 kg/m². Sustained G tolerance of 7g with an Overload Tolerance of 10g and wing break at 15g. 4× LERXs with pitch of ±40° and 2× canards with pitch of ±30° and 2× elevators with pitch of -30°


(M model adds 3D thrust vectoring with ±15° in roll/yaw and ±8° in pitch with deflection at 60 deg/s) 


Aircraft Turn Rates 


Sustained turn rates 


Mach ~1.5 Speeds 

● 1-2 deg/s at 5 km altitude 

● 2-5 deg/s at sea level   


Mach ~1 Speeds 

● 5-6 deg/s at 10 km altitude 

● 7-9 deg/s at 5 km altitude 

● 9-12 deg/s at sea level   


Mach ~0.5 Speeds 

● 8-10 deg/s at 10 km altitude 

● 11-14 deg/s at 5 km altitude 

● 15-19 deg/s at sea level   


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 8-9 deg/s at 10 km altitude 

● 10-12 deg/s at 5 km altitude 

● 13-15 deg/s at sea level 


Mach ~1 Speeds 

● 10-12 deg/s at 10 km altitude 

● 12-15 deg/s at 5 km altitude 

● 14-18 deg/s at sea level 


Mach ~0.5 Speeds 

● 12-15 deg/s at 10 km altitude 

● 14-18 deg/s at 5 km altitude 

● 20-25 deg/s at sea level 


M model adds 


Sustained turn rates 


Mach ~1.5 Speeds 

● 1-2 deg/s at 10 km altitude 

● 3-5 deg/s at 5 km altitude 

● 5-8 deg/s at sea level   


Mach ~1 Speeds 

● 7-8 deg/s at 10 km altitude 

● 10-12 deg/s at 5 km altitude 

● 13-16 deg/s at sea level   


Mach ~0.5 Speeds 

● 9-11 deg/s at 10 km altitude 

● 13-16 deg/s at 5 km altitude 

● 20-24 deg/s at sea level   


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 6-7 deg/s at 10 km altitude 

● 9-11 deg/s at 5 km altitude 

● 13-16 deg/s at sea level 


Mach ~1 Speeds 

● 14-16 deg/s at 10 km altitude 

● 16-19 deg/s at 5 km altitude 

● 17-21 deg/s at sea level 


Mach ~0.5 Speeds 

● 19-22 deg/s at 10 km altitude 

● 22-26 deg/s at 5 km altitude 

● 29-34 deg/s at sea level 


Airframe RCS

RCS Minimum: 5m²

RCS Median: 7m²

RCS Average: 8-12m²


Navigation: PNS-10 fully computerised nav/attack suite with a SAU-10V 6× axis computerised autopilot and a PNK-11 fully digital navigation system using a Ts-061K 32x bit fully digital navigation computer using a fully digital INS utilising a ring laser gyroscope and gyrostabilized accelerometer with an accuracy of 0.04° in pitch and yaw and 0.07° in heading with an error rate of 1.3 km/ph and velocity error rate of <1 m/s with a hybridised position accuracy of <30m. RV-21 solid state radar altimeters. ARK-22 solid state ADF. RSDN-20 Alpha digital radio navigation system with DVOR and ILS with a position accuracy of 20-90m and angular accuracy of ±0.1°. SNS-85 GLONASS Global navigation satellite system with a max CEP of 5m and average CEP of 30m. V004 fully digital navigation radar. 


Flight Control: SUU-27IB fully digital flight control with an SDU-10V digital fly by wire AFCS utilising a 16x bit digital ADC. SOI-27IB 3rd Generation cockpit with 2× polychrome CRT MFDs with HOTAS control stick. ZSh-7 Flight Helmet. 


(34 Prototype adds 3× polychrome CRT MFDs)


(34 adds PNS-34 fully computerised nav/attack suite with a SAU-34 6× axis fully computerised autopilot and an SDU-34 digital fly by wire AFCS utilising a 32x bit digital ADC with an K-102 fully digital navigation system utilising a SN-3307 32x bit fully digital navigation computer using a fully digital combination INS with a digital tuning fork quartz, gimballed gyrostabilized accelerometer and ring laser gyroscope with an accuracy of 0.03° in pitch, yaw and heading with an error rate of 0.05 km/ph and velocity error rate of <0.5 m/s with a hybridised position accuracy of <10m. MFD-34 4th Generation cockpit with 3× FHD LCD MFDs. RSBN-85 Vstrecha fully digital radio navigation system with DVOR and ILS with a position accuracy of 10-20m and angular accuracy of ±0.01°. V004 fully digital navigation radar. ZSh-7AP Flight Helmet. ARK-25 digital ADF. RV-20 digital radar altimeter. A-737 GLONASS-M Global navigation satellite system with a max CEP of 2m and average CEP of 10m. (When inside former USSR airspace SDCM GNSS augmentation improves precision with a max CEP of 1m and average CEP of <4m)


(34M adds PNS-34M fully computerised nav / attack suite with a KSU-34 fully digital fly by wire AFCS utilising a 64x bit digital ADC with an IVS-34 fully digital navigation system utilising a BINS-SP2M 64x bit fully digital navigation computer using a fully digital INS utilising a ring laser gyroscope, hemispherical resonator gyroscope and fiber optic gyroscope with an accuracy of 0.005° in pitch, yaw and heading with an error rate of 0.01 km/ph and velocity error rate of <0.1 m/s with a hybridised position accuracy of <1m PPA-S/V-KNS GLONASS-K Global navigation satellite system with a max CEP of 60cm and average CEP of 3m. (When inside former USSR airspace SDCM GNSS augmentation improves precision with a max CEP of 10cm and average CEP of <1m. RSBN-85VM Vstrecha-M fully digital radio navigation system with DVOR and ILS with a position accuracy of <10m and angular accuracy of ±0.01°)


Fire Control: SUO-10V fully computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with fully digital sensors with full stability augmentation with RLPK-27IB fully digital radar targeting with an Argon-A15KM1 fully digital FCC utilising L1839VM1 32x bit CPUs performing 30-50m IPS and 600-800m FLOPS. Leninets V004 4th Generation Radar utilising an electronically steered digital X band PESA system with a slotted planar antenna array using a data fused system with programmable digital signal processing, coherent doppler filtering and signal modulation based LDSD with and pulse doppler IFF and tactical & missile data link integration with CW illumination for SARH guidance, very low false alarm rates, BIST system and fully computerised radar image displaying with simultaneous multi-mode operation, simultaneous searching tracking and guidance, radar map freezing, raid assessment, predictive flight path, non tracked target tracking, adaptive processing, automatic target recognition, air and ground based JEM and HRRP non cooperative target recognition functions and agile beam, raster, palmer, conical, sector, circular and spiral scan scanning modes utilising DBS, SAR, RBGM, GTD, GMTT, TAR, TFR, STI and MGMTI air to ground radar modes, FTT, SAR, SSD and SSTT air to sea modes and SRC/LDSD, MR, ATC, STTR, MTTR and multi target RFR based ACMs air to air radar modes with gain modulation, notch filtering, sidelobe suppression, polarization filtering, tunable frequency filters, home on jam and phase coded pulse compression ECCM with 1,344 total R/Es with HPRF power output on average being 2 kW with a 15 kW max output with 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance and 1 channel for sidelobe suppression and ECM with a noise factor of 4 dB with a 1250×850 mm antenna size. TsVB-10V fully digital ballistic computer utilising a L1839VM1 32x bit CPU enabling fully automatic digital target lead and gun and missile coursing with gun, rocket and bomb CCRP and CCIP with a bomb and rocket accuracy of <4-7m CEP at a range up to 2000m and altitudes up to 5000m and <50-100m CEP at a range up to 10,000m and altitude up to 10,000m. ILS-31 4th Generation HUD with a digital LED glass display utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with an integrated digital bombing complex utilising gun, bomb and rocket CCRP and CCIP with gun EEGS. 4th Generation Radar display with an SVD system utilising a polychrome raster image displayed on a CRT MFD with computerised target generation, ECM resolution, navigation data and aircraft flight information with data link integration. 


(34 adds Sh-141 fully computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with fully digital sensors with full stability augmentation with Kishchnik data fusion system utilising NAV, RDR, TDL, IFF and EOT information displayed on one screen and Khibiny data fusion system with RFCM, IRCM, MAW, ESM, ECM and RHAWS information displayed on one screen utilising RLPK-34 radar targeting and LTPS electro optical and laser targeting with a with a Baget-55-04.01 fully digital FCC utilising KOMDIV-32 32x bit CPUs performing 260-320m IPS and 5-10b FLOPS. Leninets V004 4th Generation Radar utilising an electronically steered digital X band PESA system with a slotted planar antenna array using a data fused system with programmable digital signal processing, coherent doppler filtering and signal modulation based LDSD with and pulse doppler IFF and tactical & missile data link integration with CW illumination for SARH guidance, very low false alarm rates, BIST system and fully computerised radar image displaying with simultaneous multi-mode operation, simultaneous searching tracking and guidance, radar map freezing, raid assessment, predictive flight path, non tracked target tracking, adaptive processing, automatic target recognition, air and ground based JEM and HRRP non cooperative target recognition functions and agile beam, raster, palmer, conical, sector, circular and spiral scan scanning modes utilising DBS, SAR, RBGM, GTD, GMTT, TAR, TFR, STI and MGMTI air to ground radar modes, FTT, SAR, SSD and SSTT air to sea modes and SRC/LDSD, MR, ATC, STTR, MTTR and multi target RFR based ACMs air to air radar modes with gain modulation, notch filtering, sidelobe suppression, polarization filtering, tunable frequency filters, home on jam and phase coded pulse compression ECCM with 1,344 total R/Es with HPRF power output on average being 2 kW with a 15 kW max output with 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance and 1 channel for sidelobe suppression and ECM with a noise factor of 4 dB with a 1250×850 mm antenna size. LTPS-34 Platan multi-channel fully digital EOTS with a 720×960p polychrome LLLTV with an infrared band of 1.06 μm utilising a laser based IR spotlight with a minimum 0.001 lux conditions required and an integrated Nd:YAG auto adjusting laser targeting system with laser rangefinding, laser designation and laser spot tracking. TsVB-34 fully digital ballistic computer utilising a L1839VM1 32x bit CPU enabling fully automatic digital target lead and gun and missile coursing with gun, rocket and bomb CCRP and CCIP with bomb and rocket accuracy of <3-5m CEP at a range up to 2000m and altitudes up to 5000m and <30-70m CEP at a range up to 10,000m and altitude up to 15,000m. 5th Generation Radar display with an SVD system utilising a high resolution full colour raster image displayed on a LCD MFD with computerised target generation, ECM resolution, navigation data and aircraft flight information with data link integration) 


(34M model adds Sh-141M fully computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with fully digital sensors with full stability augmentation with the KPrNO sensor fusion system utilising NAV, RDR, IRST, EOT, TDL, IFF, RHAWS, RFCM, IRCM, MAW, ESM and ECM information displayed on one screen with radar targeting fusion utilising RLPK-34M all digital radar targeting and LTPS electro optical, laser and infrared imaging/tracking targeting system with a SOLO-35 fully digital FCC with KOMDIV-64 64x bit 2× core CPUs performing 10-20b IPS and 150-200b FLOPS. Leninets V004M 4th Generation digital PESA radar with an electronically steered X band slotted planar array with 1,344 total R/Es. TsVB-34B fully digital ballistic computer utilising an Elbrus-8S 64x bit 8× core CPU enabling fully digitised automatic digital target lead and gun and missile coursing with gun, rocket and bomb CCRP and CCIP with a bomb and rocket accuracy of <1-3m CEP at a range up to 2000m and altitudes up to 5000m and <10-30m CEP at a range up to 10,000m and altitude up to 12,000m)

 

Communication & C2: K-DIAE digital unified communication complex with R-862/R-800 VHF/UHF and R-864 HF digital radios with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding and digital data encryption with text and voice formats utilised operating on 20 channels with data transfer speeds of 1.2 kbit/s, 10 kbit/s and 16 kbit/s with an operating communication range of 350 km with an integrated LChM FHSS system utilising up to 100 frequency hops per second and VChP CRNG encoding system with 10 round cryptographic encryption for 56 bit and 8 round cryptographic encryption for 96 bit and the TKS-2 digital information data link linked to the Voyska PVO NDCC air defence network with digital electronics, frequency hopping, ECM resistance, two way communication, digital data encryption, multi aircraft link, IFF integration, electronic countermeasure support and C2 integration utilising ground and air based computer and radar generated data exchange with pre recorded voice, text and image formats used, with data transfer speeds of 75 bit/s, 150 bit/s, 300 bit/s, 1200 bit/s, 2400 bit/s and 4800 bit/s every 2 to 10 seconds operating on 3 MHz to 300 MHz with up to 20,000 frequency hops per second on 26 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1000 km with data exchange between up to 16 aircraft. SB3541 fully digital FMC utilising MP1839L1 32x bit CPUs performing 25-50m IPS and 2-4b FLOPS with 0.8-1.2m SLOC BTsK-10M RTOS with integrated aircraft health management software, electronic countermeasure support, digital navigation software, moving map display and data sharing. 


(34 adds S-103 fully digital unified communication complex with an R-833 fully digital software defined VHF/UHF and HF radio with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding, rekeying encryption and full digital data encryption with text, image and voice formats utilised operating on 8 programmable channels and 256 frequency carriers with data transfer speeds of 16 kbit/s, 5 mbit/s and 11 mbit/s utilising an PPCh integrated FHSS and CRNG system utilising up to 1000 frequency hops per second and 7 round cryptographic encryption for 128 bit, 9 round cryptographic encryption for 192 bit and 10 round cryptographic encryption for 256 bit with an operating LOS communication range of 450 km and BLOS up to 5000 km with satellite link and the TCS-2M fully digital Tactical Data Link linked to NDMC NTsUO military command center utilising the YeESU-TZ military C4 network that organises coordination between the Voiska PVO-PRO air defence network and the PTK blue force tracking network with links to Andromeda-D, Akatsiya-E, Barnaul-T, Baikal-1ME, Universal-1E, Fundament-M and Polyana-D4M1 C2 softwares and Type-1B, Planet and VIP-117M3 data terminals with fully automated VOR, GCI and ILS with fully digital electronics, frequency hopping, ECM resistance, two way communication, navigation data, fully digital data encryption, multi aircraft link, multi platform subscription, weapons management, IFF integration, electronic countermeasure support and C4 integration utilising ground and air based computer and radar generated data exchange with pre recorded voice, text and image formats used, with data transfer speeds of 1024 bit/s, 1200 bit/s, 2.4 kbit/s, 4.8 kbit/s and 16 kbit/s every 1 to 2 seconds operating on 3 MHz to 300 MHz with up to 20,000 frequency hops per second on 26 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1500 km with data exchange between up to 20 subscribers. BTsVM-900 fully digital FMC utilising i486DX4-90 32x bit CPUs performing 2-3b IPS and 90-120b FLOPS utilising the RelMK32 1-2m SLOC RTOS using a BTsK-34 C2IS suite linked to the YeESU-TZ military C4 network with squads level blue force tracking, SATCOM integration, electronic countermeasure support, precision targeting, integrated aircraft health management software, digital navigation software, moving map display and data sharing) 


(34M adda S-107-1 fully digital unified communication complex with an R-999 fully digital software defined VHF/UHF and HF radio with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding, rekeying encryption, amplitude and phase shift keying, pulse code modulation and full digital data encryption with text, video, image and voice formats utilised operating on 99 programmable channels and 512 frequency carriers with data transfer speeds of 16 kbit/s, 10 mbit/s and 30 mbit/s utilising an integrated PPCh-B FHSS and CRNG system utilising up to 20,000 frequency hops per second and 12 round cryptographic encryption for 128 bit, 14 round cryptographic encryption for 192 bit and 16 round cryptographic encryption for 256 bit with an operating LOS communication range of 450 km and BLOS unlimited with satellite link and the OSNOD fully digital tactical data link linked to the NDMC NTsUO military command center utilising the YeESU-TZ military C4 network that organises coordination between the Kavkaz-EASS military C3I radio communication network, Voiska PVO-PRO air defence network, ASUNO-S artillery network, PTK and Svod blue force tracking networks, Glaz-Groza UAV network and the Bylina electronic warfare network with links to BARS, Orbita, Andromeda-D, Strelets-M, Sagittarius-M, Akatsiya-E, Akatsiya-M, Barnaul-T, Baikal-1ME, Universal-1E, Fundament-M and Polyana-D4M1 C2 softwares and VIP-117M3, Lvin, 4RT-S, Legend, Planet, Type-1B, Kulon-V and Baget-K data terminals with two way communication, low observability data exchange, weapons management, radio communication integration, navigation data, IFF integration, SATCOM integration, fullly digital data encryption, ECM resistance, multi aircraft link, multi platform subscription, frequency hopping, electronic countermeasure support and C4 integration utilising ground, air and sea based computer, radar and electro optically generated data exchange with high resolution text, image, and pre recorded sound formats used with live video and voice formats displayed on tactical display, with data transfer speeds of 1024 bit/s, 2048 bit/s, 40 kbit/s, 100 kbit/s and 34.4 mbit/s every 0.5 to 1 seconds operating on 300 MHz to 3 GHz with up to 80,000 frequency hops per second on 60 frequency carriers enabling a LOS data transmission range up to 500 km and BLOS up to 1500 km and unlimited range with satellite link with data exchange between up to 1800 subscribers and unlimited with satellite link. Baget-53-31M fully digital FMC with a 1888TX018 64x bit 8× core CPUs performing 20-30b IPS and 300-400b FLOPS utilising the BagrOS-4000 4-5m SLOC RTOS using an IUS C2ISR suite linked to the YeESU-TZ military C4 network with section to platoon level blue force tracking software, C4 integration, SATCOM integration, GNSS integration, electronic countermeasure support, surrounding land formation intelligence, digital navigation, moving map display, precision targeting, integrated aircraft health management software, reconnaissance software, data sharing and C2 software)


(2024 models onwards use Baget-53-31M1 fully digital FMC utilising Elbrus-16S 64x bit 16× core CPUs performing 30-40b IPS and 400-600b FLOPS for FMC) 


Targeting: V004 PESA radar with a 120° primary horizontal and ±60° vertical scan range with tracking of 10 targets and data linking of 4 missiles enabling an Rmax range up to 370 km, 300 km detection range for an aircraft with an RCS of 15m² and a track range of 120 km for an aircraft with an RCS of 3m² with a LDSD detection range of 100 km for 5m² and a LDSD track range of 60 km for an aircraft with an RCS of 5m² with a rangefinding radar gun engagement range up to 10 km with a max ground attack detection range up to 250 km and a track range for tank sized targets up to 140 km with tracking of 4 ground targets with ground mapping up to 150 km, with base image resolutions of 1.5, 10 and 30 m at a spatial resolution size of 2, 30 and 150 km with radar imaging complete in 30 seconds with a tracking scan range of 120° in azimuth and ±60° in elevation with a full scan sweep in 0.2 seconds with max tracking target velocity at over 7400 kph and stores tracking information for up to 10 non tracked targets with predictive flight paths for non tracked targets up to 12 seconds with LDSD ground clutter rejection of 80> dB. 


(34 adds Platan EOTS utilising a fully digital telescopic electro optical sight with a angular FOV of 45°, 30× optical magnification with an angular FOV of 1.5° and a 60× electro optical magnification with an angular FOV of 0.75° with an independent stabilised vertical movement of -170°/+0° and independent stabilised horizontal movement of 70° with a moving stabilisation accuracy of 0.1 in elevation and azimuth and minimum/maximum stabilised sight movements of 0.02/40 deg/s with an angular tracking rate of 60 deg/s with tracking of up to 10 targets with LLLTV enabling a max range of 55 km, detection of tank sized targets up to 33 km and identification up to 29 km with detection of corvette sized warships up to 52 km with identification up to 48 km with automatic target tracking up to 20 km and laser targeting with laser rangefinding, laser designation and laser spot tracking with an accuracy of ±5m with with a 30 km engagement range for ground targets) 


(34M model adds V004M PESA radar with SAR imaging up to 250 km, with base image resolutions of 1, 5 and 10 m at a spatial resolution size of 50, 150 and 250 km with radar imaging complete in 30 seconds)


Targeting Pods 

APK-9 Tekon data link pod for live video feed of Kh-29 and Kh-59 seekers. 



M400 Series Targeting Pods for 34 


M402 Pika 2nd Generation Targeting Pod with a 2nd Generation SLAR radar with a PESA slotted planar array utilising ~1000 AL R/E modules with a horizontal scan range of 150° and vertical scan range of 90° with SAR imaging up to 100 km, with base image resolutions of 1, 5 and 10 m at a spatial resolution size of 20, 50 and 100 km with radar imaging complete in 30 seconds with tracking of up to 10 targets. 


M400 Sapsan 2nd Generation Targeting Pod with a FHD resolution TV sight with a ~1080p day time image resolution, Raduga-III 2nd Generation FLIR system utilising a 1PN99M matrix with a 576x2 FPA format, 768×576p thermal image resolution, 8-12 μm spectral range, pixel pitch of 30 μm, NETp of 70 mK and 50 Hz refresh rate and an Nd:YAG laser targeting system with laser rangefinding, laser designation and laser spot tracking with an accuracy of 10m with with a utilising a fully digital telescopic electro optical sight with a day time 4× optical magnification with an FOV of 18.5°, 30× optical magnification with a FOV of 2.5° and a 60× electro optical magnification with an FOV of 1.2° with a night time 1× optical magnification with an FOV of 18°, 8× optical magnification with a FOV of 2.2° and a 16× optical magnification with an FOV of 1.1° with independent stabilised depth movement, an independent stabilised vertical movement of -150°/+10° and independent stabilised horizontal movement of 180° with a moving stabilisation accuracy of ±0.1 in elevation and azimuth and minimum/ maximum stabilised sight movements of 0.02/60 deg/s with an angular tracking rate of 40 to 60 deg/s with tracking of up to 20 targets and locking of up to 4 with FLIR enabling a max range of 30 km, detection of tank sized targets up to 10 km and identification up to 2.5 km with detection of corvette sized warships up to 25 km with identification up to 17 km with detection of fighter sized targets up to 18 km and identification up to 3 km, TV sight enabling a max range of 60 km, detection of tank sized targets up to 42 km and identification up to 36 km with detection of corvette sized warships up to 57 km with identification up to 52 km with a 30 km laser engagement range for ground targets.



BKR-3 Targeting Pod Family for Su-34M 


UKR-OE 3rd Generation Targeting Pod for high altitude reconnaissance with an integrated automatic adjustment laser designator with a Antrakt-TV UHD resolution day time TV sight with ~1440p day time resolution and Raduga-VM 3rd Generation FLIR system utilising a 1PN147 matrix with a 640x512 FPA format, 1280×1024p thermal image resolution, 3-5 μm spectral range, pixel pitch of 15 μm, NETp of 25 mK and 50 Hz refresh rate format with a EOTS with FLIR enabling a max range of 40 km, detection of tank sized targets up to 15 km and identification up to 4 km with detection of corvette sized warships up to 32 km with identification up to 22 km with detection of fighter sized targets up to 23 km and identification up to 5 km, TV sight enabling a max range of 120 km, detection of tank sized targets up to 90 km and identification up to 80 km with detection of corvette sized warships up to 100 km with identification up to 90 km with automatic target tracking up to 10 km and LDR with a 40 km engagement range for ground targets with tracking of 60 targets. 


UKR-RL Pika-M 3rd Generation Targeting Pod with an FGA-51-2/3 Zhuk-AU 3rd Generation X/P band SLAR radar with two AESA patch antenna arrays each with 900 GaAs T/R modules with a total horizontal scan range of 300° and a vertical scan range of 60° with SAR imaging up to 300 km, with base image resolutions of 0.3, 0.5 and 1.5 m at a spatial resolution size of 100, 200 and 300 km with radar imaging complete in 20 seconds and 2× FGA-51-1 Zhuk-AU 4th Generation GARs utilising an electronically steered fully digital X band AESA system with a patch antenna array using a sensor fused system with programmable fully digital signal processing, digital beam forming, coherent doppler filtering, signal modulation and STI based LDSD with CW illumination for SARH guidance and very low false alarm rates with a fully computerised radar image displayed utilising DBS I/SAR, RBGM, STI, GTD, TAR, TFR and MGMTI air to ground radar modes with automatic target recognition, notch filtering, sidelobe suppression, polarization filtering, adaptive processing, frequency hopping, home on jam and phase coded pulse compression ECCM each array has 1000 GaAs T/R modules with a 120° horizontal and ±60° vertical scan range enabling a 300 km Rmax range, with a max ground detection range of 300 km and 80 km track range for tank sized targets with tracking of up to 20 ground targets. 


Counter Measures: L-150/SPO-32 Pastel 3rd Generation fully digital RHAWS with 16 targets tracked and 128> preprogrammed threat identifiers with guidance of up to 6 ARMs with 2 fired simultaneous and 10× receivers enabling a self protection envelope of 360° in azimuth and ±60° in elevation with band coverage of 1.2-18 GHz with a signal detectability range up to 320 km. SSP-2I digital fire countermeasure system. K-36DM Zero-Zero ejection seat. APP-50 countermeasure dispenser utilising 1st Generation IRCM and RFCM with 192 total rounds using the PPR-50 composite aluminium chaff that activates in 0.3 seconds and creates a false target RCS of greater than 60m² and using the PPI-50 thermite based flare with a minimum burn time of 3 seconds. SO-72/SRZO-2P 2nd Generation digital IFF interrogator / transponder linked to the Parol-2D fully digital IFF system with aircraft ID, full digital data encryption, radio/inertial navigation locating, reprogramming and cryptographic encoding. P-591 digital ICAS. KKO-15LP digital full ECLSS. Armoured cockpit with resistance against 30×165mm API and glass resistant to 14.5×114mm. 


(34 adds L-150NU-34/SPO-32M Pastel-M 4th Generation fully digital data fused RHAWS with 20 targets tracked with 242> preprogrammed threat identifiers with guidance of up to 8 ARMs with 4 fired simultaneous with 16× receivers enabling a self protection envelope of 360° in azimuth and ±180° in elevation with band coverage of 0.2-20 GHz with a signal detectability range up to 440 km. SO-96/SRZ-035M 3rd Generation fully digital IFF interrogator / transponder linked to the Parol-2D fully digital IFF system with aircraft ID, full digital data encryption, radio/inertial navigation locating, reprogramming and cryptographic encoding. APP-50M countermeasure dispenser utilising 2nd Generation IRCM and RFCM with 192 total rounds using the PPR-50-17 composite aluminium jammer assisted chaff that activates in 0.3 seconds and creates a false target RCS of greater than 60m² and using the PPI-50-3 spectral flare with a minimum burn time of 3 seconds. N012 Rassvet PESA tail warning radar with a missile detection range up to 20 km and 50 km track range vs RCS of 3m² and max detection range of 100 km)


(34M model adds SOZhE-35 fully digital ICAS, full ECLSS and fire countermeasure system and K-36D-5 Zero-Zero ejection seats. UV-50 countermeasure dispensers utilising 2nd Generation IRCM and 3rd Generation RFCM with 168 total rounds using PPR-50-17-110V composite aluminium jammer assisted chaff that activates in 0.3 seconds and creates a false target RCS of greater than 60m², PPI-50-3 spectral flare with a minimum burn time of 3 seconds and Lobushka disposable DRFM jammers with a jamming time up to 6 seconds. Blesna Diamant-S 3rd Generation RFCM with a towed decoy SPJ with a 100m towing range utilising simultaneous LPIR, monopulse, continuous wave and pulse doppler countermeasure. Kopyo-DL AESA tail warning radar with a missile detection range up to 50 km and 80 km track range vs RCS of 3m² and max detection range of 200 km)


(From early 2020s onwards Parol-2D is replaced by Password-3 all digital IFF system with aircraft ID, low observability data sharing, satellite navigation locating, full digital data encryption, reprogramming and cryptographic encoding)


Electronic Warfare: L-005S Sorbitsya-S 3rd Generation digital SPJ with monopulse countermeasure, continuous wave countermeasure and pulse doppler countermeasure ECCM with track breaker, track breaking and blip enhancement ELINT with 4× receivers enabling an ECCM protection envelope of 360° in azimuth with a self protection jamming range of 200 km> with SPS-171 3rd Generation digital active jamming system operating on 6-10 GHz with deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, cross eye jamming and spot jamming jamming ECM with 4× PESA pyramidal horn antenna ECM transmitters enabling an active jamming range of 200 km>


(34 model adds L-175V Khibiny-10V 4th Generation fully digital SPJ utilising radio direction finder with AoA and PRF determination, simultaneous monopulse countermeasure, continuous wave countermeasure, pulse doppler countermeasure and LPIR countermeasure with doppler shifting, home on jam and anti burn though ECCM with track breaker, advanced decoy generation, blip enhancement and global navigation spoofing ELINT with 6× receivers enabling a passive ECCM protection envelope of 360° in azimuth with a self protection jamming range of 300 km> with SAP-518 4th Generation fully digital active jamming system operating on 5-18 GHz with frequency agile deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, cross eye jamming, spot jamming, wave jamming, power managed jamming and DRFM jamming ECM with 4× GaAs AESA pyramidal horn antenna ECM transmitters enabling an active jamming range of 300 km>) 


(34M models add L-265M10-02 Khibiny-MV 5th Generation fully digital ECM System with an SPJ suite utilising radio direction finder with AoA and PRF determination, simultaneous monopulse countermeasure, continuous wave countermeasure, pulse doppler countermeasure and LPIR countermeasure with doppler shifting, noise cloaking, home on jam, anti burn though and self jam resistance ECCM with track breaker, advanced decoy generation, blip enhancement, satellite interception and global navigation spoofing ELINT with 8× receivers enabling a passive ECCM protection envelope of 360° in azimuth with a self protection jamming range of 400 km> with SAP-518SM 5th Generation fully digital active jamming system operating on 2-20 GHz with frequency agile deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, interrupted jamming, cross eye jamming, spot jamming, wave jamming, power managed jamming and DRFM/ISRJ jamming ECM with 4× GaN AESA pyramidal horn antenna array ECM transmitters enabling an active jamming range of 400 km>.)


Guns: GSh-30-1 30mm autocannon slaved to radar and laser rangefinder with an effective firing range up to 2 km. 


Ordinance Capacity: 12× hardpoints with a max 14,000 kg munition capacity and 180 rounds for the gun. 


Common Air to Air Payloads 

8× R-77 2× R-73M/R-27ET 


R-77

4th Generation Radar Missile 

9P-1348 Inverse Monopulse X band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a radio correction data link with back up inertial operting guidance, home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a Z23nA radio proximity fuse and back up impact detonation with with a high explosive blast warhead enabling a blast radius of 10-15 m²

~150 km max Range at 10 km+ altitude 

~120 km max Range at 5 km+ altitude 

~58 km max Range at sea level 

~35 km engagement range vs RCS of 5m² at sea level 

~80 km engagement range vs RCS of 5m² at 5 km+ altitude 

~110 km engagement range vs RCS of 5m² at 10 km+ altitude 

~15 km NEZ range vs RCS of 5m² at sea level 

~25 km NEZ range vs RCS of 5m² at 5 km> altitude

~30 km NEZ range vs RCS of 5m² at 10 km> altitude

~8 km ARH lock range vs RCS of 1m²

~14 km ARH lock range vs RCS of 5m²

~22 km ARH lock range vs RCS of 10m²

~0.1 m² minimum target RCS for ARH lock 

~Mach 4 at high altitude 

~Mach 3 at sea level 

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~50g Overload Tolerance 

~8g launch limiter

~10g target limiter 


R-27ER

3rd Generation Radar Missile 

9B-1101E Inverse Monopulse X band Semi Active Seeker with a fully digital phase comparison antenna array with an INS utilising a radio correction data link with back up inertial operting guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a radio proximity fuse and back up impact detonation with a continuous rod warhead enabling a blast radius of 10-15 m²

~130 km max Range at 10 km+ altitude 

~110 km max Range at 5 km+ altitude 

~90 km max Range at sea level 

~70 km engagement range vs RCS of 5m² at sea level 

~90 km engagement range vs RCS of 5m² at 5 km+ altitude 

~110 km engagement range vs RCS of 5m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 5m² at sea level 

~30 km NEZ range vs RCS of 5m² at 5 km> altitude

~50 km NEZ range vs RCS of 5m² at 10 km> altitude

~Mach 5 at 10 km+ altitude 

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Targeting Angles 35°

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~60g Overload Tolerance 

~8g launch limiter 

~10g target limiter 


R-27ET 

4th Generation IR Missile 

Geofizika-36TE LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~120 km max Range at altitude 

~40 km max Range at sea level 

~80 km engagement range 

~All aspect lock range 20 km

~Rear aspect lock range 30 km

~Mach 4 at 10 km+ altitude 

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Rectile Speed: 125 Hz

~Flare rejection 0.6

~Gimbal limit: 55°

~Angular Tracking: 60 deg/s 

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 60g 


R-74

4th Generation IR Missile 

Mayak-80B LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~30 km max Range at 5 km> altitude 

~20 km max Range at sea level 

~20 km engagement range at 5 km>

~All aspect lock range 6 km

~Rear aspect lock range 10 km

~Mach 3 at 5 km> altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.6

~Gimbal limit: 60°

~Angular Tracking: 60 deg/s 

~Turn Rate 90 to 120 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 60g 


Laser Guided Bombs 

KAB-1500L 1st Generation LG HE  

KAB-1500L-Pr-E 2nd Gen Bunker Buster 

KAB-1500L-F-E 1st Generation FRAG-HE 

KAB-1500L-OD-E 1st Generation FAE 

KAB-1500L-K-E 1st Generation Cluster Bomb 

KAB-500L 1st Generation LG HE  

KAB-500L-Pr-E 2nd Gen Bunker Buster 

KAB-500L-F-E 1st Generation FRAG-HE 

KAB-500L-OD-E 1st Generation FAE 

KAB-500L-K-E 1st Generation Cluster Bomb 


Optically Guided Bombs 

KAB-1500Kr-Pr-E 2nd Gen Bunker buster 

KAB-1500Kr-F-E 2nd Generation FRAG-HE 

KAB-1500Kr-OD-E 2nd Generation FAE 

KAB-1500TK 2nd Generation MITL HE 

KAB-1500Kr 2nd Generation HE

KAB-500Kr 2nd Generation HE

KAB-500Kr-Pr-E 2nd Gen Bunker Buster 

KAB-500Kr-F-E 2nd Generation FRAG-HE 

KAB-500Kr-OD-E 2nd Generation FAE 

KAB-500Kr-K-E 2nd Generation Cluster Bomb


Land Attack Missiles 

Kh-25ML-M 2nd Generation Laser Guided HE 

Kh-25ML-F 2nd Gen Laser Guided FRAG-HE 

Kh-25MT-M 2nd Generation OG HE 

Kh-25MT-F 2nd Generation OG FRAG-HE 

Kh-25MTP-M 2nd Generation OG/IIR HE 

Kh-25MTP-F 2nd Generation OG/IIR FRAG-HE 

Kh-59-M 3rd Generation HE Cruise Missile

Kh-59-K 3rd Generation HEAT Cruise Missile

Kh-59-KE 3rd Gen Cluster Cruise Missile

Kh-59L-M 2nd Gen Laser Guided HE

Kh-59L-K 2nd Gen Laser Guided HEAT

Kh-59L-KE 2nd Gen Laser Guided Cluster 

Kh-59T-M 2nd Generation OG HE

Kh-59T-K 2nd Generation OG HEAT

Kh-59T-KE 2nd Generation OG Cluster 

Kh-29T-M 2nd Generation OG HE

Kh-29T-K 2nd Generation OG HEAT 

Kh-29L-M 2nd Generation Laser Guided HE 

Kh-29L-K 2nd Generation Laser Guided HEAT 

Kh-31A 3rd Generation Anti Ship 

Kh-31P 2nd Generation Anti Radiation 

Kh-58 2nd Generation Anti Radiation  


Unguided Bombs 

FAB-500 HE bomb

FAB-250  HE bomb

BETAB-500 bunker buster

RBK-500 cluster munition bomb

RBK-250 cluster munition bomb

KMGU cluster munition dispenser 


Rockets

S-24 HE-FRAG Rocket


B-13L Rocket Pod

S-5M HE-FRAG Rocket 

S-5K HEAT Rocket 

S-5S Flechette Rocket 


B-8M1 Rocket Pod

S-8S Flechette rocket 

S-8P chaff rocket 

S-8D FAE rocket 

S-8KO HEAT Rocket 

S-8B Bunker buster rocket 


UB-32 Rocket Pod 

S-13 KEP Rocket 

S-13T HEAT Rocket 


Common Payloads for Su-34


2× Kh-59L 2× Kh-29L 2× KAB-500L 2× R-77-1 2× R-74M 2× SAP-518

4× Kh-29D 2× Kh-38MT 2× R-77-1 2× R-74M 2× SAP-518

2× Kh-31PD 4× Kh-58U 2× R-77-1 2× R-74M 2× SAP-518

4× Kh-59MK2 4× Kh-60 2× Kh-59M2 2× R-74M 2× SAP-518

2× Kh-41 4× Kh-31AD 2× R-74M 2× SAP-518

4× Kh-35U 4× Kh-59MK 2× R-77-1 2× R-74M 2× SAP-518

1× Kh-47M2 4× R-77-1 2× R-74M 2× SAP-518


R-77-1B

4+ Generation Radar Missile 

9B-1103M-150 Inverse Monopulse X/Ku band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a bi-directional radio correction data link with back up inertial operting guidance, dual band, home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser and Z23nA radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~200 km max Range at 10 km+ altitude 

~150 km max Range at 5 km+ altitude 

~80 km max Range at sea level 

~50 km engagement range vs RCS of 5m² at sea level 

~110 km engagement range vs RCS of 5m² at 5 km+ altitude 

~140 km engagement range vs RCS of 5m² at 10 km+ altitude 

~30 km NEZ range vs RCS of 5m² at sea level 

~40 km NEZ range vs RCS of 5m² at 5 km> altitude

~60 km NEZ range vs RCS of 5m² at 10 km> altitude

~8 km ARH lock range vs RCS of 1m²

~20 km ARH lock range vs RCS of 5m²

~26 km ARH lock range vs RCS of 10m²

~0.05 m² minimum target RCS for ARH lock 

~Mach 5 max target velocity 

~Mach 4 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~Launch limiter 9g 

~Target limiter 12g 

~Overload Tolerance 60g


R-27ET 

4th Generation IR Missile 

Geofizika-36TE LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~120 km max Range at altitude 

~40 km max Range at sea level 

~80 km engagement range 

~All aspect lock range 20 km

~Rear aspect lock range 30 km

~Mach 4 at 10 km+ altitude 

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Rectile Speed: 125 Hz

~Flare rejection 0.6

~Gimbal limit: 55°

~Angular Tracking: 60 deg/s 

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 60g 


R-74M

4+ Generation IR Missile 

Impuls-90 LN² Cooled NIR & UV channel all digital pseudo-imaging HgCdTe Seeker with dual band, gatewidth and seeker shut off IRCCM

~50 km max Range at 5 km> altitude 

~40 km max Range at sea level 

~40 km engagement range at 5 km> altitude

~All aspect lock range 10 km

~Rear aspect lock range 10 km 

~Mach 3 at 5 km> altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.8

~Gimbal limit: 75°

~Angular Tracking: 60 deg/s 

~Turn Rate 120 to 180 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 80g 


Air to Ground Missiles  

Kh-101 LO 4th Gen HE Cruise Missile 

Kh-101 LO 4th Gen Cluster Cruise Missile 

Kh-69 LO 4th Gen Cluster Cruise Missile 

Kh-69 LO 4th Gen HEAT Cruise Missile 

Kh-59MK2-F-E LO 3rd Gen OG/IIR FRAG-HE 

Kh-59M2-M 2nd Generation OG HE 

Kh-59M2-K 2nd Generation OG HEAT 

Kh-59M2-KE 2nd Generation OG Cluster 

Kh-59M2D-M 2nd Generation OG/IIR HE 

Kh-59M2D-K 2nd Generation OG/IIR HEAT 

Kh-59M2D-KE 2nd Generation OG/IIR Cluster 

Kh-59MK-M 4th Generation HE Cruise Missile

Kh-59MK-K 4th Gen HEAT Cruise Missile

Kh-59MK-KE 4th Gen Cluster Cruise Missile

Kh-58UShKE 3rd Gen Anti Radiation  

Kh-58UShKE-TP 3rd Gen OG/IIR Anti Radiation

Kh-55U 4th Gen HE Cruise Missile 

Kh-SD LO 4th Gen HE Cruise Missile 

Kh-47M2 5th Generation HE Ballistic Missile

Kh-38MA-M 4th Gen HE Ballistic Missile 

Kh-38MA-K 4th Gen HEAT Ballistic Missile

Kh-38MA-KE 4th Gen Cluster Ballistic Missile

Kh-38ML-M 3rd Generation Laser Guided HE 

Kh-38ML-K 3rd Gen Laser Guided HEAT

Kh-38ML-KE 3rd Gen Laser Guided Cluster 

Kh-38MT-M 3rd Generation OG/IIR HE 

Kh-38MT-K 3rd Gen OG/IIR HEAT

Kh-38MT-KE 3rd Gen OG/IIR Cluster  

Kh-36 4th Generation FRAG-HE Glide Missile 

Kh-32 4th Generation HE Anti Ship Missile 

Kh-31PD 3rd Generation Anti Radiation 

Kh-29MP-M 4th Gen HE Ballistic Missile 

Kh-29MP-K 4th Gen HEAT Ballistic Missile 

Kh-29TE-M 3rd Generation OG HE 

Kh-29TE-K 3rd Generation OG HEAT 

Kh-29TD-M 3rd Generation OG/IIR HE 

Kh-29TD-K 3rd Generation OG/IIR HEAT 

Kh-29ML-M 3rd Generation Laser Guided HE 

Kh-29ML-K 3rd Gen Laser Guided HEAT   

Kh-25ML-M 2nd Generation Laser Guided HE 

Kh-25ML-F 2nd Gen Laser Guided FRAG-HE 

Kh-25MT-M 2nd Generation OG HE 

Kh-25MT-F 2nd Generation OG FRAG-HE 


Laser Guided Bombs 

KAB-20LG-K 3rd Generation HEAT 

KAB-20LG-FE 3rd Generation FRAG-HE  

KAB-50LG-K 3rd Generation HEAT 

KAB-50LG-FE 3rd Generation FRAG-HE  

KAB-100LG-K 3rd Generation HEAT 

KAB-100LG-FE 3rd Generation FRAG-HE 

KAB-250LG 3rd Generation HE 

KAB-250LG-F-E 3rd Generation FRAG-HE 

KAB-250LG-OD-E 3rd Generation FAE

KAB-500MLG 3rd Generation HE

KAB-500MLG-Pr-E 3rd Gen Bunker Buster 

KAB-500MLG-F-E 3rd Generation FRAG-HE 

KAB-500MLG-OD-E 3rd Generation FAE 

KAB-500MLG-K-E 3rd Gen Cluster Bomb

KAB-1500MLG 3rd Generation HE

KAB-1500MLG-Pr-E 3rd Gen Bunker Buster 

KAB-1500MLG-F-E 3rd Generation FRAG-HE 

KAB-1500MLG-OD-E 3rd Generation FAE 

KAB-1500MLG-K-E 3rd Gen Cluster Bomb


Optically Guided Bombs 

KAB-50Kr-M-K 3rd Generation HEAT 

KAB-50Kr-MT-K 3rd Generation IIR HEAT 

KAB-50Kr-M-FE 3rd Generation FRAG-HE 

KAB-50Kr-MT-FE 3rd Generation IIR FRAG-HE 

KAB-100Kr-M-K 3rd Generation HEAT 

KAB-100Kr-MT-K 3rd Generation IIR HEAT 

KAB-100Kr-M-FE 3rd Generation FRAG-HE 

KAB-100Kr-MT-FE 3rd Gen IIR FRAG-HE

KAB-250Kr-M 3rd Generation HE 

KAB-250Kr-M-F-E 3rd Generation FRAG-HE 

KAB-250Kr-M-OD-E 3rd Generation FAE

KAB-500Kr-M 3rd Generation HE

KAB-500Kr-M-Pr-E 3rd Gen Bunker Buster 

KAB-500Kr-M-F-E 3rd Generation FRAG-HE 

KAB-500Kr-M-OD-E 3rd Generation FAE 

KAB-500Kr-M-K-E 3rd Gen Cluster Bomb

KAB-1500Kr-M 3rd Generation HE

KAB-1500Kr-M-Pr-E 3rd Gen Bunker Buster 

KAB-1500Kr-M-F-E 3rd Generation FRAG-HE 

KAB-1500Kr-M-OD-E 3rd Generation FAE 

KAB-1500Kr-M-K-E 3rd Gen Cluster Bomb


Bunker Busters 

Kh-59MKM 3rd Generation Bunker Buster 

Kh-59MK2-Pr LO 3rd Gen Bunker Buster 

KAB-1500Kr-Pr-E 3rd Gen Bunker buster 

KAB-1500LG-Pr-E 3rd Gen Bunker buster 

KAB-500Kr-Pr-E 2nd Gen Bunker Buster 

KAB-500LG-Pr-E 2nd Gen Bunker Buster

KAB-250LG-Pr-E 2nd Gen Bunker Buster

FAB-500T 1st Generation Bunker buster 

FAB-1500T 1st Generation Bunker buster

BETAB-500SHP 1st Generation bunker buster

BETAB-500 1st Generation Bunker buster 

BETAB-500Y 1st Generation Bunker buster 


Satellite Guided Munitions 

Kh-25MS-M Satellite guided HE 

Kh-25MS-F Satellite guided FRAG-HE 

Kh-38MK-M Satellite Guided HE 

Kh-38MK-K Satellite Guided HEAT

Kh-38MK-KE Satellite Guided Cluster 

KAB-20S-E satellite guided HE bomb 

KAB-50S-E Satellite guided HE bomb 

KAB-100S-E satellite guided HE bomb 

KAB-250S-E satellite guided HE bomb 

KAB-500S-E Satellite guided HE bomb 

KAB-1500S-E satellite guided HE bomb

KAB-500Kr UMPK Satellite guided TV bomb 

ZAB-100 UMPK satellite guided Incen bomb 

ZAB-250 UMPK satellite guided Incen bomb

ODAB-500 UMPK satellite guided FAE bomb 

ODAB-1500 UMPK satellite guided FAE bomb 

RBK-500 UMPK satellite guided cluster bomb

FAB-250 UMPK satellite guided HE bomb 

FAB-500 UMPK satellite guided HE bomb 

FAB-1500 UMPK satellite guided HE bomb 

FAB-250 UMPB satellite guided HE bomb 

FAB-500 UMPB satellite guided HE bomb 

FAB-1500 UMPB satellite guided HE bomb


Unguided Bombs 

FAB-250 Unguided HE Bomb 

FAB-500 Unguided HE Bomb 

FAB-1500 Unguided HE Bomb 

FAB-2000 Unguided HE Bomb 

FAB-3000 Unguided HE Bomb 

FAB-5000 Unguided HE Bomb 

OFAB-150 Unguided Frag Bomb 

OFAB-250 Unguided Frag Bomb 

OFAB-500 Unguided Frag Bomb 

PLAB-250-120 Unguided ASW bomb 

ZAB-100-105 Unguided Incendiary bomb

ZAB-250-200 Unguided Incendiary bomb 

ODAB-500 Unguided fuel air bomb 

PTAB-500 Unguided anti tank bomb 

PTAB-500Y Unguided Anti Tank bomb 


Rockets 

S-5M HE rocket 

S-5K HEAT rocket 

S-5S KEP rocket 

S-5Kor 2nd Gen laser guided rocket 

S-8T Tandem HEAT rocket 

S-8OFP1 HE-FRAG-PEN rocket 

S-8BM 2nd Gen Bunker buster rocket 

S-8DF FAE rocket 

S-8Kor 2nd Gen laser guided rocket

S-13Kor 2nd Gen laser guided rocket

S-13DF FAE rocket 

S-13OF APAM-FRAG rocket 

S-13T Tandem HEAT Rocket 

S-13B 2nd Gen Bunker buster rocket 

S-24 HE-FRAG rocket

S-25-OFM 2nd Gen Bunker buster rocket 

S-25L 1st Gen laser guided rocket

S-25-O FRAG-HE rocket 


GSh-6-23

9A-620 23×115mm HEI

9A-620 23×115mm HE-T

9A-620 23×115mm AP-T

9A-620 23×115mm SAPHEI

9A-620 23×115mm MKETF


Later models add 


R-77-1C

4+ Generation Radar Missile 

9B-1103M-200PA Inverse Monopulse Ku band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a bi-directional radio correction data link with back up inertial operting guidance, home on jam, multimode guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser and Z23nA radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~200 km max Range at 10 km+ altitude 

~150 km max Range at 5 km+ altitude 

~80 km max Range at sea level 

~50 km engagement range vs RCS of 3m² at sea level 

~100 km engagement range vs RCS of 3m² at 5 km+ altitude 

~120 km engagement range vs RCS of 3m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 3m² at sea level 

~40 km NEZ range vs RCS of 3m² at 5 km> altitude

~60 km NEZ range vs RCS of 3m² at 10 km> altitude

~10 km ARH lock range vs RCS of 1m²

~20 km ARH lock range vs RCS of 3m²

~30 km ARH lock range vs RCS of 10m²

~0.05 m² minimum target RCS for ARH lock 

~Mach 5 max target velocity 

~Mach 4 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~Launch limiter 9g 

~Target limiter 12g 

~Overload Tolerance 60g


M model adds 


R-77M

5th Generation Radar Missile 

9B-1103M2 Ka/Ku band AESA Active Seeker with 64 GaAs T/R modules using an fully digital patch antenna array with an INS/GNSS utilising a bi-directional radio correction data link with back up inertial operting guidance, LPIR, home on jam, dual band seeker and polarisation filtering ECCM utilising a solid fuel dual pulse rocket motor with a laser and radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~300 km max Range at 10 km+ 

~250 km max Range at 5 km+

~150 km max Range at sea level 

~120 km engagement range vs RCS of 1m² at sea level 

~190 km engagement range vs RCS of 1m² at 5 km+ altitude 

~220 km engagement range vs RCS of 1m² at 10 km+ altitude 

~50 km NEZ range vs RCS of 1m² at sea level 

~70 km NEZ range vs RCS of 1m² at 5 km> altitude

~90 km NEZ range vs RCS of 1m² at 10 km> altitude

~2 km ARH lock range vs RCS of 0.003m²

~14 km ARH lock range vs RCS of 1m²

~26 km ARH lock range vs RCS of 3m²

~35 km ARH lock range vs RCS of 10m²

~0.0005 m² minimum target RCS for ARH lock 

~90 km NEZ range vs RCS of 1m²

~Mach 6 max target velocity 

~Mach 5 top speed above 5 km altitude 

~Mach 3 top speed at sea level

~Targeting Angles 60°

~Turn Rate 70 to 120 Deg/s

~Initial Acceleration of 300-600 m/s>

~Launch limiter 10g 

~Target limiter 12g 

~Overload Tolerance 80g


R-37M

4+ Generation Radar Missile 

9B-1103M-350 Inverse Monopulse Ku/X band Active Seeker with an fully digital slotted planar antenna array with an INS/GNSS utilising a bi-directional radio correction data link with back up inertial operting guidance, home on jam, dual band seeker and polarisation filtering ECCM utilising a solid fuel dual pulse rocket motor with a kolibri radio proximity fuse with back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-20 m²

~400 km max range at 10 km+ altitude 

~300 km max Range at 5 km+ altitude 

~150 km max Range at sea level 

~120 km engagement range vs RCS of 3m² at sea level 

~200 km engagement range vs RCS of 3m² at 5 km+ altitude 

~300 km engagement range vs RCS of 3m² at 10 km+ altitude 

~70 km NEZ range vs RCS of 3m² at sea level 

~90 km NEZ range vs RCS of 3m² at 5 km> altitude

~120 km NEZ range vs RCS of 3m² at 10 km> altitude

~20 km ARH lock range vs RCS of 1m²

~40 km ARH lock range vs RCS of 3m²

~70 km ARH lock range vs RCS of 10m²

~0.005 m² minimum target RCS for ARH lock 

~Targeting Angles 45°

~Turn Rate 10 to 30 Deg/s

~Initial Acceleration of 600-900 m/s>

~8g launch limiter

~8g target limiter 

~40g overload tolerance 

~Mach 6 max target velocity 

~Mach 6 top speed above 5 km altitude 

~Mach 4 top speed at sea level


R-74M2

4th Generation IR Missile 

Karfagen-760 LN² Cooled MIR & UV channel fully digital pseudo-imaging HgCdTe LOAL Seeker with dual band, MITL, IOG, gatewidth and seeker shut off IRCCM

~60 km max Range 

~50 km range at sea level 

~50 km engagement range 

~All aspect lock range 10 km

~Rear aspect lock range 10 km

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Flare rejection 0.9+

~Turn Rate 120 to 180 Deg/s

~Initial Acceleration of 300-400 m/s>

~Rectile Speed: 200 Hz

~Gimbal limit: 180°

~Angular Tracking: 75 deg/s 

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 80g



Su-32 


Su-32FN 

Su-34 (Prototype) 


Su-34 (Production) 


Su-34M








Su-30 Series 

Su-30 / Su-27PU

Prototype: 1989

Aircraft Role: MultiRole/Intercepter

Generation: 4th

Number Built: 5+


Su-30K

Prototype: 1992

Aircraft Role: MultiRole/Strike Fighter 

Generation: 4+

Number Built: 2

Combat Rank: D


Su-30M

Prototype: 1992

Completed: 1994

Production: 1996

Service: 1998

Aircraft Role: MultiRole 

Generation: 4+

Number Built: 550+

Combat Rank: A


Su-30SM

Prototype: 1998

Completed: 2009

Production: 2013

Service: 2019

Aircraft Role: MultiRole/Strike Fighter 

Generation: 4+

Number Built: 100+

Combat Rank: S


Su-30SM2

Prototype: 2018

Completed: 2021

Production: 2022

Service: 2024

Aircraft Role: MultiRole/Strike Aircraft 

Generation: 4.5 

Number Made: 80+


Engine and Airframe: CAD designed Composite construction with an RCS minimum of 4m². Crew of 2. Length 22 m. Height 5.9 m. Wingspan 15.3 m. Wing area 62 m². Frame weight 19,000 kg. Takeoff weight 34,500 kg. Max Fuel 11,500 kg. 2× Lyul'ka-Saturn AL-31-SM axial flow high bypass turbofans with a digital electronic engine control with 160 kN of thrust and 250 kN in afterburner. 


(SM model adds CAD designed Composite construction with an RCS minimum of 4m². creww of 2. Length 21.9 m. Height 6.4 m. Wingspan 14.7 m. Wing area 62 m². Frame weight 17,700 kg. Takeoff weight 34,400 kg. Max Fuel 9400 kg. 2× Lyul'ka-Saturn AL-31-FP axial flow high bypass turbofans with a digital electronic engine control with 150 kN of thrust and 246 kN in afterburner. Refueling boom)


Speed and Endurance: Top speed of mach 2 to 2.4 at 15 km+, mach 2 to 2.2 at 10 km+, mach 1.8 to 2 to at 5 km+ and mach 1 to 1.2 at sea level. Service Ceiling of 18 to 20 km. Combat range of 1000-1500 km. Acceleration 10-19 seconds to mach 1 at sea level. Stall speed 190-280 kph. Take off distance is 500m with ATA payload to 900m for full payload. Landing distance 700 to 900m. In flight refueling. 


(SM2 model adds 2× Lyul'ka-Saturn AL-41-F1S 3D thrust vectoring variable bypass axial flow FADEC turbofans with supercruise. Top speed of mach 2.2 to 2.5 at 15 km+, mach 2 to 2.4 at 10 km+, mach 2 to 2.2 to at 5 km+ and mach 1 to 1.3 at sea level with supercruise at mach 1.1 at sea level and mach 1.3 at 10 km+. Service Ceiling of 19 to 22 km) 


Manuvarabilities: Thrust to weight ratio of 1.1 at full air to air payload and 1.5 at half fuel/loadout and 0.9 at full loadout. Roll rate of 160 deg/s at high speed and 230 deg/s at low speed. Climb rate of 280-320 m/s. No AOA limit at low speeds with 59° angle of attack at mach 1>.  10 to 20 kph/s speed bleed at high g instantaneous maneuvers and 10 to 30 kph/s speed bleed at high g sustained maneuvers. Sustained G tolerance of 9g with an Overload Tolerance of 13g and wing break at 19.5-26g. Wing loading of 370-420 kg/m. 4× LERXs with pitch of ±40° and 2× canards with pitch of ±30° and 2× elevators with pitch of -30°


(SM model adds 3D thrust vectoring with ±15° in pitch/roll and ±3.5° in yaw with deflection at 30 deg/s. Thrust to weight ratio of 1 at full air to air payload and 1.2 at half fuel/loadout and 0.8 at full loadout. Roll rate of 180 deg/s at high speed and 230 deg/s at low speed. Climb rate of 220-270 m/s. No AOA limit at any speed. 10 to 20 kph/s speed bleed at high g instantaneous maneuvers and 10 to 20 kph/s speed bleed at high g sustained maneuvers. Wing loading of 390-470 kg/m². Sustained G tolerance of 9g and a max Overload Tolerance of 13g and wing break at 19.5-26g. 4× LERXs with pitch of ±40° and 2× canards with pitch of ±30°and 2× elevators with pitch of -30°) 


(SM2 models add 3D thrust vectoring with ±15° in roll/yaw and ±8° in pitch with deflection at 60 deg/s. No AOA limit at any speed)


Airframe RCS

RCS Minimum: 4m²

RCS Median: 5m²

RCS Average: 7-10m²


Aircraft Turn Rates 


SM model adds 


Sustained turn rates 


Mach ~1.5 Speeds 

● 3-4 deg/s at 10 km altitude 

● 4-6 deg/s at 5 km altitude 

● 5-8 deg/s at sea level  


Mach ~1 Speeds 

● 9-10 deg/s at 10 km altitude 

● 11-13 deg/s at 5 km altitude 

● 13-16 deg/s at sea level  


Mach ~0.5 Speeds 

● 18-20 deg/s at 10 km altitude 

● 20-23 deg/s at 5 km altitude 

● 24-28 deg/s at sea level 


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 6-7 deg/s at 10 km altitude 

● 8-10 deg/s at 5 km altitude 

● 10-13 deg/s at sea level  


Mach ~1 Speeds 

● 16-18 deg/s at 10 km altitude 

● 19-22 deg/s at 5 km altitude 

● 24-28 deg/s at sea level  


Mach ~0.5 Speeds 

● 25-28 deg/s at 10 km altitude 

● 28-32 deg/s at 5 km altitude 

● 30-35 deg/s at sea level  



SM2 model adds 


Sustained turn rates 


Mach ~1.5 Speeds 

● 6-7 deg/s at 10 km altitude 

● 8-10 deg/s at 5 km altitude 

● 10-13 deg/s at sea level  


Mach ~1 Speeds 

● 10-11 deg/s at 10 km altitude 

● 13-15 deg/s at 5 km altitude 

● 16-19 deg/s at sea level  


Mach ~0.5 Speeds 

● 18-20 deg/s at 10 km altitude 

● 22-25 deg/s at 5 km altitude 

● 26-30 deg/s at sea level  


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 11-12 deg/s at 10 km altitude 

● 12-14 deg/s at 5 km altitude 

● 14-17 deg/s at sea level  


Mach ~1 Speeds 

● 23-25 deg/s at 10 km altitude 

● 26-29 deg/s at 5 km altitude 

● 28-32 deg/s at sea level  


Mach ~0.5 Speeds 

● 25-28 deg/s at 10 km altitude 

● 30-34 deg/s at 5 km altitude 

● 37-42 deg/s at sea level  


Navigation: PrNK-10 computerised navigation suite with a SAU-10 3× axis computerised autopilot and an SDU-10 analogue fly by wire AFCS utilising a SVS-2Ts-2 4x bit digital ADC with a 50-100k SLOC-OS with navigation systems, electronic flight control and autopilot link. PNK-10-02 digital navigation system with a Ts-050 8x bit digital navigation computer using IP-1-72A/IS-1-72A digital INS with a digital tuning fork quartz and gyrostabilized accelerometer with an accuracy of 0.1° in pitch and yaw and 0.2° in heading with an error rate of 3.5 km/ph and velocity error rate of <3 m/s. SOI-10 2nd Generation cockpit with 1× CRT MFD and HOTAS control stick. RV-21 solid state radar altimeters. ARK-22 solid state ADF. RSDN-20 Alpha digital radio navigation system with DVOR and ILS with a position accuracy of 20-90m and angular accuracy of ±0.1°. ZSh-5 Flight Helmet. 


Flight Control: SDU-10 analogue fly by wire AFCS utilising a Ts-080-1 16x bit digital ADC. ZSh-7 Flight Helmet. SOI-27 3rd Generation cockpit with 2× polychrome CRT MFDs and TV sight with a HOTAS control stick.


(SM model adds PNS-30 fully computerised nav/attack suite with a SAU-10-30 6× axis computerised autopilot and a SDU-30 digital fly by wire AFCS utilising a 32x bit digital ADC with an LINS-100RS fully digital navigation system utilising a Sigma-95N 32x bit fully digital navigation computer using a fully digital INS utilising a ring laser gyroscope, digital tuning fork quartz INS and gyrostabilized accelerometer with an accuracy of 0.03° in pitch and yaw and 0.05° in heading with an error rate of 0.09 km/ph and velocity error rate of <0.5 m/s with a hybridised position accuracy of <10m. SMD-55 4th Generation cockpit with 7× FHD LCD MFDs and HOTAS control stick. RSBN-85 Vstrecha fully digital radio navigation system with DVOR and ILS with a position accuracy of 10-20m and angular accuracy of ±0.01°. ZSh-7AP Flight Helmet. ARK-25 digital ADF. RV-21 digital radar altimeter. A-737 GLONASS-M Global navigation satellite system with a max CEP of 2m and average CEP of 10m. N011M-R navigation radar)


Fire Control: SUO-27P computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with digital sensors with stability augmentation with the OEPrNK-10 data fusion system utilising NAV, IFF, RDR, IDL and IRST information displayed on one screen with RLPK-27 radar targeting system and OEPS-27 laser and infrared tracking targeting system with a Ts-101M digital FCC utilising K1801 16x bit CPUs performing 300-400k IPS and 150-200m FLOPS. N001V Mech-V 3rd Generation X band mechanically steered solid state long chord twist cassegrain antenna array using analogue to digital signal processing, coherent doppler filtering based LDSD with and pulse doppler IFF and tactical & missile data link integration with CW illumination for SARH guidance, reduced false alarm rates and computerised radar image displaying with multi-mode operation, predictive flight path and non tracked target tracking functions and raster, conical, sector, circular and spiral scan scanning modes utilising SRC/LDSD, STTR, MTTR and HMD, LDR, IRST and RFR based ACMs air to air radar modes with gain modulation, polarization filtering and pulse compression ECCM with HPRF power output on average being 1 kW with a 8 kW max output with 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance and 1 channel for sidelobe suppression and ECM with a noise factor of 6 dB with a 1074 mm antenna diameter. ILS-31 4th Generation HUD with a digital LED glass display utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with an integrated digital bombing complex utilising gun, bomb and rocket CCRP and CCIP with gun EEGS. IPV 4th Generation Radar display with an SVD system utilising a polychrome raster image displayed on a CRT MFD with computerised target generation, ECM resolution, navigation data and aircraft flight information with data link integration. ZSh-5 Helmet with Shchel-3UM 1st Generation HMD. OLS-27 2nd Generation IRST with a LN² cooled pseudoimaging InSb detector and 12P2-01 1.06 μm Nd:YAG laser rangefinder. TsVBM-10 digital ballistic computer utilising a 580VM80 8x bit CPU enabling gun and missile coursing. 


(K model adds RLPU-27M fully computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with fully digital sensors with full stability augmentation with RLPK-27 radar targeting and OEPS-27M electro optical, laser and infrared imaging/tracking targeting utilising OEPrNK-10 data fusion system utilising NAV, IFF, RDR, IDL and IRST information displayed on one screen with a Ts-200 fully digital FCC utilising M1839 32x bit CPUs performing 50-75m IPS and 600-800m FLOPS. N011 Bars 4th Generation Radar with a digital X band mechanically steered monopulse system with a slotted planar antenna array using a data fused system with programmable digital signal processing, coherent doppler filtering and signal modulation based LDSD with and pulse doppler IFF and tactical & missile data link integration with CW illumination for SARH guidance, low false alarm rates and computerised radar image displaying with multi-mode operation, radar map freezing, raid assessment, predictive flight path, non tracked target tracking, BIST system, air based JEM non cooperative target recognition functions and raster, conical, sector, circular and spiral scan scanning modes utilising GTD, GTT, TAR and TFR air to ground radar modes and SRC/LDSD, MR, STTR, MTTR and HMD, LDR, IRST, EOT and multi target RFR based ACMs air to air radar modes with gain modulation, notch filtering, low sidelobe antenna, polarization filtering and pulse compression ECCM with HPRF power output on average being 2 kW with a 10 kW max output with 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance and 1 channel for sidelobe suppression and ECM with a noise factor of 4 dB with a 960 mm antenna diameter. OLS-27K 2nd Generation IRST with a LN² cooled pseudoimaging InSb detector with an integrated 1.06 μm Nd:YAG laser rangefinder. ZSh-5 Flight Helmet with Shchel-3UM 1st Generation HMD utilising automatic cueing for targeting with head tracking software. IPV-1 4th Generation Radar display with an SVD system utilising a polychrome raster image displayed on a CRT MFD with computerised target generation, ECM resolution, navigation data and aircraft flight information with data link integration. ILS-31 4th Generation HUD with a digital LED glass display utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with an integrated digital bombing complex utilising gun, bomb and rocket CCRP and CCIP with gun EEGS)


(SM model adds Bars-R fully computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with fully digital sensors with full stability augmentation with RLPK-30 radar targeting and OEPS-30 electro optical, laser and infrared imaging/tracking targeting utilising OEPrNK-30 data fusion system utilising IFF, NAV, RDR, IRST, EOT and TDL information displayed on one screen information displayed on one screen and Khibiny data fusion system with RFCM, IRCM, MAW, ESM, ECM and RHAWS information displayed on one screen with a Ts-200M fully digital FCC utilising KOMDIV-32 32x bit CPUs performing 260-320m IPS and 5-10b FLOPS. N011M-R Bars-R 4+ Generation Radar with a mechanically and electronically steered digital X band Hybrid PESA system with an L band beacon interrogator with a slotted planar antenna array using a data fused system with programmable digital signal processing, hybrid beam forming, coherent doppler filtering and signal modulation based LDSD with and pulse doppler IFF and tactical & missile data link integration with CW illumination for SARH guidance, low false alarm rates and fully computerised radar image displaying with multi-mode operation, simultaneous searching tracking and guidance, radar map freezing, raid assessment, predictive flight path, non tracked target tracking, adaptive processing, automatic target recognition, BIST system, air and ground based JEM, RCS and HRRP non cooperative target recognition functions and raster, conical, sector, circular and spiral scan scanning modes utilising DBS, SAR, RBGM, GTD, GMTT, TAR, TFR, STI and GMTI air to ground radar modes, SAR, SSD and SSTT air to sea modes and SRC/LDSD, MR, STTR, MTTR and HMD, LDR, IRST, EOT and multi target RFR based ACMs air to air radar modes with gain modulation, notch filtering, sidelobe suppression, polarization filtering and phase coded pulse compression ECCM with HPRF power output on average being 1-2 kW with a 7 kW max output with a 960 mm antenna diameter with 1,660 R/Es broken up into 20 T/R modules utilising a EGSP-6A chelnok TWT transmitter and 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance and 1 channel for sidelobe suppression and ECM with a noise factor of 3.5 dB. ZSH-7AP Flight Helmet with NSTs-T-04 1st Generation HMD utilising automatic cueing for targeting with head tracking software. 5th Generation Radar display with an SVD system utilising a high resolution full colour raster image displayed on a LCD MFD with computerised target generation, ECM resolution, navigation data and aircraft flight information with data link integration. CTH-3022 5th Generation HUD with a fully digital LCD glass display utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with an integrated digital bombing complex utilising gun, bomb and rocket CCRP and CCIP with gun EEGS and a digital MFD with electro optical slaving, mission control, navigation systems and weapons functions. OLS-30 multi-channel fully digital EOTS with a HD resolution TV sight with a ~720p day time image resolution, 1.06 μm Nd:YAG laser targeting system with laser rangefinding, laser designation and laser spot tracking and a 2nd Generation IRST & 2nd Generation FLIR system utilising a LN² cooled infrared imaging InSb detector with an FPA format of 96x4 and a thermal image resolution of 576×480p. TsVB-90 fully digital ballistic computer utilising a L1839VM1 32x bit CPU enabling fully automatic digital target lead and gun and missile coursing with gun, rocket and bomb CCRP and CCIP with a bomb and rocket accuracy of <4-7m CEP at a range up to 2000m and altitudes up to 5000m and <50-100m CEP at a range up to 10,000m and altitude up to 10,000m)


Communication & C2: K-DIAE digital unified communication complex with R-862/R-800 VHF/UHF and R-864 HF digital radios with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding and digital data encryption with text and voice formats utilised operating on 20 channels with data transfer speeds of 1.2 kbit/s, 10 kbit/s and 16 kbit/s with an operating communication range of 350 km with an integrated LChM FHSS system utilising up to 100 frequency hops per second and VChP CRNG encoding system with 10 round cryptographic encryption for 56 bit and 8 round cryptographic encryption for 96 bit and the TKS-2 digital information data link linked to the Voyska PVO NDCC air defence network with digital electronics, frequency hopping, ECM resistance, two way communication, digital data encryption, multi aircraft link, IFF integration, electronic countermeasure support and C2 integration utilising ground and air based computer and radar generated data exchange with pre recorded voice, text and image formats used, with data transfer speeds of 75 bit/s, 150 bit/s, 300 bit/s, 1200 bit/s, 2400 bit/s and 4800 bit/s every 2 to 10 seconds operating on 3 MHz to 300 MHz with up to 20,000 frequency hops per second on 26 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1000 km with data exchange between up to 16 aircraft. Rubezh-M digital GCI complex with the Spektr-1 and Biryusa digital navigation data links and BAN-75, SVPK, SPK-75 and SPK-68 digital command data links connected to the SAU-10 computerised autopilot, ARK-22 solid state ADF, SO-69 solid state IFF interrogator and SRZO-2P solid state IFF transponder linked to the PVO NDCC air defence network with fully automated ground controlled interception, weapons management, IFF integration, digital data encryption and navigation data utilising ground based computer and radar generated data exchange with pre recorded voice and text formats used with data transfer speeds of 45 bit/s, 80 bit/s and 96 bit/s every 5 to 10 seconds operating on 2 MHz to 400 MHz with up to 1000 frequency hops per second on 10 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1000 km with data exchange between up to 36 aircraft.


(K/M model adds TsVM-90-6 fully digital FMC utilising MP1839L1 32x bit CPUs performing 25-50m IPS and 2-4b FLOPS with a 600-800k SLOC BTSK-10 RTOS with integrated aircraft health management software, electronic countermeasure support, digital navigation software, moving map display and data sharing)


(SM model adds S-103 fully digital unified communication complex with an R-833 fully digital software defined VHF/UHF and HF radio with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding, rekeying encryption and full digital data encryption with text, image and voice formats utilised operating on 8 programmable channels and 256 frequency carriers with data transfer speeds of 16 kbit/s, 5 mbit/s and 11 mbit/s utilising an PPCh integrated FHSS and CRNG system utilising up to 1000 frequency hops per second and 7 round cryptographic encryption for 128 bit, 9 round cryptographic encryption for 192 bit and 10 round cryptographic encryption for 256 bit with an operating LOS communication range of 450 km and BLOS up to 5000 km with satellite link and the TCS-2M fully digital Tactical Data Link linked to NDMC NTsUO military command center utilising the YeESU-TZ military C4 network that organises coordination between the Voiska PVO-PRO air defence network and the PTK blue force tracking network with links to Andromeda-D, Akatsiya-E, Barnaul-T, Baikal-1ME, Universal-1E, Fundament-M and Polyana-D4M1 C2 softwares and Type-1B, Planet and VIP-117M3 data terminals with fully automated VOR, GCI and ILS with fully digital electronics, frequency hopping, ECM resistance, two way communication, navigation data, fully digital data encryption, multi aircraft link, multi platform subscription, weapons management, IFF integration, electronic countermeasure support and C4 integration utilising ground and air based computer and radar generated data exchange with pre recorded voice, text and image formats used, with data transfer speeds of 1024 bit/s, 1200 bit/s, 2.4 kbit/s, 4.8 kbit/s and 16 kbit/s every 1 to 2 seconds operating on 3 MHz to 300 MHz with up to 20,000 frequency hops per second on 26 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1500 km with data exchange between up to 20 subscribers. BTsVM-900 fully digital FMC utilising i486DX4-90 32x bit CPUs performing 2-3b IPS and 90-120b FLOPS utilising the RelMK32 1-2m SLOC RTOS using a BTsK-30 C2IS suite linked to the YeESU-TZ military C4 network with squads level blue force tracking, SATCOM integration, electronic countermeasure support, precision targeting, integrated aircraft health management software, digital navigation software, moving map display and data sharing) 


(2024 SM2 models onwards use Baget-53-31M1 fully digital FMC utilising Elbrus-16S 64x bit 16× core CPUs performing 30-40b IPS and 400-600b FLOPS for FMC) 


(SM2 adds Adaptation-Su upgrade with Sh-135 fully computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with fully digital sensors with full stability augmentation with the KPrNO-35 sensor fusion system utilising NAV, RDR, IRST, EOT, TDL, IFF, RHAWS, RFCM, IRCM, MAW, ESM and ECM information displayed on one screen with radar targeting fusion with an RLPK-35S/OEPS-35S fully digital radar, laser, electro optical and infrared imaging/tracking targeting system with a SOLO-35 fully digital FCC with KOMDIV-64 64x bit 2× core CPUs performing 10-20b IPS and 150-200b FLOPS, utilising all digital flight control system and the Baget-53-31M fully digital FMC with a 1888TX018 64x bit 8× core CPUs performing 20-30b IPS and 300-400b FLOPS utilising the BagrOS-4000 4-5m SLOC RTOS using an IUS-35 C2ISR suite linked to the YeESU-TZ military C4 network with section to platoon level blue force tracking software, C4 integration, SATCOM integration, GNSS integration, electronic countermeasure support, surrounding land formation intelligence, digital navigation, moving map display, precision targeting, integrated aircraft health management software, reconnaissance software, data sharing and C2 software, TsVB-54 fully digital ballistic computer utilising a KOMDIV-64 64x bit 2× core CPU enabling fully digitised automatic digital target lead with gun, rocket and bomb CCRP and CCIP with a bomb and rocket accuracy of <3-5m CEP at a range up to 2000m and altitudes up to 5000m and <30-40m CEP at a range up to 10,000m and altitude up to 12,000m, RSBN-85VM Vstrecha-M fully digital radio navigation system with DVOR and ILS with a position accuracy of <10m and angular accuracy of ±0.01°, KPrNO-35 fully computerised nav/attack suite with a SAU-35 6× axis computerised autopilot and a KSU-35 fully digital fly by wire AFCS utilising a 64x bit digital ADC with an IVS-35 fully digital navigation system utilising a BINS-SP2 64x bit fully digital navigation computer using a fully digital combination INS with a digital tuning fork quartz, gimballed gyrostabilized accelerometer and ring laser gyroscope with an accuracy of 0.03° in pitch, yaw and heading with an error rate of 0.05 S-107-1 fully digital unified communication complex with an R-999 fully digital software defined VHF/UHF and HF radio with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding, rekeying encryption, amplitude and phase shift keying, pulse code modulation and full digital data encryption with text, video, image and voice formats utilised operating on 99 programmable channels and 512 frequency carriers with data transfer speeds of 16 kbit/s, 10 mbit/s and 30 mbit/s utilising an integrated PPCh-B FHSS and CRNG system utilising up to 20,000 frequency hops per second and 12 round cryptographic encryption for 128 bit, 14 round cryptographic encryption for 192 bit and 16 round cryptographic encryption for 256 bit with an operating LOS communication range of 450 km and BLOS unlimited with satellite link and the OSNOD fully digital tactical data link linked to the NDMC NTsUO military command center utilising the YeESU-TZ military C4 network that organises coordination between the Kavkaz-EASS military C3I radio communication network, Voiska PVO-PRO air defence network, ASUNO-S artillery network, PTK and Svod blue force tracking networks, Glaz-Groza UAV network and the Bylina electronic warfare network with links to BARS, Orbita, Andromeda-D, Strelets-M, Sagittarius-M, Akatsiya-E, Akatsiya-M, Barnaul-T, Baikal-1ME, Universal-1E, Fundament-M and Polyana-D4M1 C2 softwares and VIP-117M3, Lvin, 4RT-S, Legend, Planet, Type-1B, Kulon-V and Baget-K data terminals with two way communication, low observability data exchange, weapons management, radio communication integration, navigation data, IFF integration, SATCOM integration, fullly digital data encryption, ECM resistance, multi aircraft link, multi platform subscription, frequency hopping, electronic countermeasure support and C4 integration utilising ground, air and sea based computer, radar and electro optically generated data exchange with high resolution text, image, and pre recorded sound formats used with live video and voice formats displayed on tactical display, with data transfer speeds of 1024 bit/s, 2048 bit/s, 40 kbit/s, 100 kbit/s and 34.4 mbit/s every 0.5 to 1 seconds operating on 300 MHz to 3 GHz with up to 80,000 frequency hops per second on 60 frequency carriers enabling a LOS data transmission range up to 500 km and BLOS up to 1500 km and unlimited range with satellite link with data exchange between up to 1800 subscribers and unlimited with satellite link.. N035 Irbis 5th Generation Radar utilising a mechanically and electronically steered fully digital X band Hybrid PESA system with a slotted planar antenna array using a sensor fused system with programmable fully digital signal processing, hybrid beam forming, coherent doppler filtering and signal modulation based LDSD with and pulse doppler IFF and tactical & missile data link integration with CW illumination for SARH guidance, very low false alarm rates, BIST system and fully computerised radar image displaying with simultaneous multi-mode operation, simultaneous searching tracking and guidance, radar map freezing, raid assessment, predictive flight path, non tracked target tracking, adaptive processing, automatic target recognition, multi target air and ground based SAR, JEM, RCS and HRRP non cooperative target recognition functions and raster, conical, sector, circular and spiral scan scanning modes utilising DBS, I/SAR, RBGM, GTD, MGMTT, TAR, TFR, STI and MGMTI air to ground radar modes, FTT, I/SAR, SSD and SSTT air to sea modes and SRC/LDSD, MR, LPIR, ATC, STTR, MTTR and HMD, LDR, IRST, EOT and multi target RFR based ACMs air to air radar modes with gain modulation, notch filtering, sidelobe suppression, polarization filtering, tunable frequency filters, frequency hopping, home on jam, jammer identification and phase coded pulse compression ECCM with 1,840 R/Es broken up into 20 T/R modules utilising two EGSP-27 chelnok TWT transmitters and 4 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance, 1 channel for sidelobe suppression and ECM and 1 channel for FHSS waveform engagement with a 900 mm diameter antenna size and a HPRF power output on average being 5-7 kW with a 20 kW max output. 2× N036Sh Pokosnik 5th Generation electronically steered L band AESA radars with a quad radiator antenna array using a sensor fused system with programmable fully digital signal processing utilising low observability beacon interrogation and pulse doppler IFF integration with very low false alarm rates with a fully computerised radar image displayed with multi-mode operation, predictive flight path and non tracked target tracking functions and agile beam and spiral scan scanning modes utilising SRC, LPIR, MTTR and STTR radar modes with sidelobe suppression, polarization filtering, frequency hopping and phase coded pulse compression ECCM with 48 GaAs T/R modules with a ~1100×100 mm antenna size with a HPRF power output on average being 8-12 kW with a 48 kW max output. OLS-35 multi-channel fully digital EOTS with a HD resolution TV sight with a ~1080p day time image resolution, 1.06 μm Nd:YAG auto adjusting laser targeting system with laser rangefinding, laser designation and laser spot tracking and a 3rd Generation IRST & 3rd Generation FLIR system utilising a LN² cooled infrared imaging HgCdTe detector with an FPA format of 384x388 and a thermal image resolution of 776×768p, IKSh-1M 5th Generation fully digital HUD with an integrated fully digital bombing complex with gun, bomb and rocket CCRP and CCIP with full gun EEGS, ZSh-7AP Flight Helmet with NSTsI-KOS 2nd Generation HMD utilising automatic cueing for targeting with navigation data and weapons management data displayed with head tracking and PPA-S/V-KNS GLONASS-K Global navigation satellite system with a max accuracy of 60cm and average accuracy of 3m) 


Targeting Systems: Mech-V radar with 120° horizontal and -55°/+60° vertical scan range enabling tracking of up to 10 targets and data linking of 2 missiles with a Rmax range up to 200 km, 140 km detection range for 16m² RCS and track range of 80 km for 3m² RCS with a LDSD detection range of 40-50 km for 16m² and a LDSD track range of 30-45 km for an aircraft with an RCS of 3m² with a rangefinding radar gun engagement range up to 10 km with a tracking scan range of 80° in azimuth and -15°/+25° in elevation and a tracking scan time of 5 seconds with max tracking target velocity at over 2500 kph and stores tracking information for up to 2 non tracked target with predictive flight paths for non tracked targets up to 10 seconds with LDSD ground clutter rejection of 60> dB and low chaff rejection with a MTBF of 60 to 100 hours. 


(K model adds Bars radar with a 180° horizontal scan range and ±90° vertical scan range enabling tracking of up to 12 targets and data linking of 4 missiles with with an Rmax range up to 400 km, 350 km detection range for 16m² and 150 km track range for an aircraft with an RCS of 5m² with a LDSD detection range of 120 km for 5m² and a LDSD track range of 80 km for an aircraft with an RCS of 5m² with a rangefinding radar gun engagement range up to 10 km with a 200 km ground detection range with a 60 km track range for tank sized targets with tracking of up to 4 ground targets with ground mapping up to 200 km, with base image resolutions of 100, 1000 and 3000 m at a spatial resolution size of 10, 100 and 200 km with radar imaging complete in 40 seconds with a tracking scan range of 120° in azimuth and ±30° in elevation and a scan time of 2 seconds with max tracking target velocity at over 4000 kph and stores tracking information for up to 10 non tracked target with predictive flight paths for non tracked targets up to 12 seconds with LDSD ground clutter rejection of 80> dB, NCTR with up to 1 target up to 30 km with a scan range of ±15° in azimuth and ±5° in elevation with up to 20 preprogrammed target identifiers and high chaff rejection with a MTBF of 100 to 200 hours. OLS-27K IRST with tracking of up to 2 targets and automatic target tracking with an angular resolution of 0.1° and max tracking rate of 120 deg/s enabling a max detection range up to 100 km with a 50 to 80 km detection range and 20 to 40 km rear track range with 15 km front track range for fighter sized targets and laser targeting system with laser rangefinding with an accuracy of 10m and a 8 km engagement range for aircraft with a horizontal FOV up to 120° and a vertical FOV of -15°/+60°. Shchel-3UM HMD with a 120° horizontal FOV and ±30° vertical FOV up to 10 km)


(SM model adds Bars-R radar with a horizontal scan range of 170° and ±90° vertical scan range enabling tracking of up to 15 targets and data linking of 6 missiles with an Rmax range of 400 km, in 15-24° STTR narrow beam mode detection range is 300 to 400 km vs RCS of 5m², 200 to 300 km vs RCS of 3m² and 90 to 120 km vs RCS of 1m², normal detection range 350 km for 16m² with track range of 200 km vs aircraft with an RCS of 5m² with a LDSD detection range of 150 km for 5m² and a LDSD track range of 110 km for an aircraft with an RCS of 3m² with a rangefinding radar gun engagement range up to 10 km with a max ground attack detection range up to 200 km and a track range for tank sized targets up to 50 km with tracking of 9 targets and locking of up to 3 with ground mapping up to 200 km, with base image resolutions of 1, 10 and 30 m at a spatial resolution size of 1, 90 and 200 km with radar imaging complete in 30 seconds with a tracking scan range of 140° in azimuth and ±40° in elevation with a tracking scan sweep in 0.2 seconds with max tracking target velocity at over 7408 kph and stores tracking information for up to 10 non tracked targets with predictive flight paths for non tracked targets up to 13 seconds with LDSD ground clutter rejection of 90> dB, NCTR for 1 target up to 30 km with a scan range of ±15° in azimuth and ±5° in elevation with up to 50 preprogrammed target identifiers and high chaff rejection with a MTBF of 200 to 300 hours. OLS-30 fully stabilised sight with a fully digital electro optical system with a 4× optical magnification with an FOV of 18.75° and a 10× optical magnification with an FOV of 7.5° with an independent stabilised vertical movement of -15°/+30° and independent stabilised horizontal movement of 120° with a moving stabilisation accuracy of 0.1 mils in azimuth and elevation and minimum/maximum stabilised sight movements of 0.03/60 deg/s with an angular tracking rate of 10 to 20 deg/s with FLIR enabling a max range of 20 km, detection of tank sized targets up to 10 km and identification up to 2 km with detection of corvette sized warships up to 16 km with identification up to 10 km with detection of fighter sized targets up to 13 km and identification up to 2 km, TV sight enabling a max range of 15 km with detection of tank sized targets up to 8 km and identification up to 6 km with detection of fighter sized targets up to 10 km and identification up to 8 km with NFOV detection of corvette sized warships up to 13 km with identification up to 11 km, IRST with tracking of up to 2 targets and automatic target tracking with an angular resolution of 0.1° and max tracking rate of 120 deg/s enabling a max detection range up to 120 km with a 70 to 100 km detection range and 20 to 40 km rear track range with 15 km front track range for fighter sized targets and a 20 km track range for ground targets and laser targeting with laser rangefinding, laser designation and laser spot tracking with an accuracy of 5m with a 15 km engagement range for aircraft and 20 km engagement range for ground targets. NSTs-T-04 HMD with a 140° horizontal FOV and -35°/+65° vertical FOV with a target engagement range up to 10 km)


Targeting Pods 

APK-9 Tekon data link pod for live video feed of Kh-29 and Kh-59 seekers. 


Targeting Pods for SM models 


M400 Sapsan 2nd Generation Targeting Pod with a FHD resolution TV sight with a ~1080p day time image resolution, Raduga-III 2nd Generation FLIR system utilising a 1PN99M matrix with a 576x2 FPA format, 768×576p thermal image resolution, 8-12 μm spectral range, pixel pitch of 30 μm, NETp of 70 mK and 50 Hz refresh rate and an Nd:YAG laser targeting system with laser rangefinding, laser designation and laser spot tracking with an accuracy of 5 to 10m with with a utilising a fully digital telescopic electro optical sight with a day time 4× optical magnification with an FOV of 18.5°, 30× optical magnification with a FOV of 2.5° and a 60× electro optical magnification with an FOV of 1.2° with a night time 1× optical magnification with an FOV of 18°, 8× optical magnification with a FOV of 2.2° and a 16× optical magnification with an FOV of 1.1° with independent stabilised depth movement, an independent stabilised vertical movement of -150°/+10° and independent stabilised horizontal movement of 180° with a moving stabilisation accuracy of 0.1 in elevation and azimuth and minimum/ maximum stabilised sight movements of 0.02/60 deg/s with an angular tracking rate of 40 to 60 deg/s with tracking of up to 20 targets and locking of up to 4 with FLIR enabling a max range of 30 km, detection of tank sized targets up to 10 km and identification up to 2.5 km with detection of corvette sized warships up to 25 km with identification up to 17 km with detection of fighter sized targets up to 18 km and identification up to 3 km, TV sight enabling a max range of 60 km, detection of tank sized targets up to 42 km and identification up to 36 km with detection of corvette sized warships up to 57 km with identification up to 52 km with a 30 km laser engagement range for ground targets.


SM2 Targeting Pods 

T-220I 3rd Generation Targeting Pod with UHD EOTS with a ~1440p day time image resolution, Raduga-V 3rd Generation FLIR system utilising a 1PN136 matrix with a 388x384 FPA format, 776×768p thermal image resolution, 3-5 μm spectral range, pixel pitch of 15 μm, NETp of 30 mK and 50 Hz refresh rate with an integrated auto adjusting Nd:YAG laser targeting system with laser rangefinding, laser designation and laser spot tracking with an accuracy of 1 to 10m with utilising a fully digital telescopic electro optical sight with a day time 4× optical magnification with an FOV of 25°, 60× optical magnification with an FOV of 1.6° and a 120× electro optical magnification with an FOV of 0.8° with a night time 1× optical magnification with an FOV of 24°, 10× optical magnification with an FOV of 2.4° and a 20× optical magnification with an FOV of 1.2° with independent stabilised depth movement, an independent stabilised vertical movement of -170°/+10° and independent stabilised horizontal movement of 320° with a moving stabilisation accuracy of 0.05 in elevation and azimuth and minimum/ maximum stabilised sight movements of 0.01/60 deg/s with an angular tracking rate of 50 to 90 deg/s with tracking of up to 30 targets and locking of up to 8 with FLIR enabling a max range of 30 km, detection of tank sized targets up to 12 km and identification up to 3 km with detection of corvette sized warships up to 28 km with identification up to 20 km with detection of fighter sized targets up to 20 km and identification up to 4 km with automatic target tracking up to 8km , TV sight enabling a max range of 90 km, detection of tank sized targets up to 50 km and identification up to 45 km with detection of fighter sized targets up to 70 km and identification up to 60 km with detection of corvette sized warships up to 87 km with identification up to 80 km with a 40 km laser engagement range for ground targets. 


(SM2 adds Irbis radar with a 245° horizontal and ±120° vertical scan range enabling tracking of up to 30 targets and data linking of 8 missiles with a 400 km Rmax range, in 15-24° narrow beam mode detection range is 350 to 400 km vs RCS of 3m², 250 to 300 km vs RCS of 1m² and 80 to 100 km vs RCS of 0.01m², normal detection range of 400 km vs RCS of 5m² and track range of 200 km vs RCS of 3m² with a LDSD detection range of 250 km for 5m² and a LDSD track range of 200 km for an aircraft with an RCS of 3m² with a rangefinding radar gun engagement range up to 20 km with a max ground attack detection range up to 300 km and a track range for tank sized targets up to 90 km with tracking of 4 ground targets with ground mapping up to 300 km, with base image resolutions of 1, 3 and 10 m at a spatial resolution size of 100, 200 and 300 km with radar imaging complete in 30 seconds with a tracking scan range of 125° in azimuth and ±60° in elevation with a scan sweep in 0.2 seconds with max tracking target velocity at over 7408 kph and LPI target acquisition with over 300 frequency hops per second and a max LPI engagement range of 200 km vs RCS of 3m² and stores tracking information for up to 15 non tracked targets with predictive flight paths for non tracked targets up to 14 seconds with LDSD ground clutter rejection of 100> dB, NCTR for 2 targets up to 60> km with a scan range of ±30° in azimuth and ±15° in elevation with up to 120 preprogrammed target identifiers and high chaff rejection with a MTBF of 400 to 600 hours. N036Sh AESA radars have a 180° horizontal scan range with a 500 km Rmax range, 400 km detection range for 3m² and 150 km track range for 0.1m². X/L band Radar Data fused targeting with a horizontal scan range of 245° and a ±120° vertical scan range enabling tracking of up to 30 targets and data linking of 8 missiles with an Rmax range up to 500 km, 400 km detection range for an aircraft with an RCS of 3m² and track range of 200 km for an aircraft with an RCS of 1m². OLS-35 fully stabilised sight with a fully digital electro optical system with a 4× optical magnification with an FOV of 18.75° and a 10× optical magnification with an FOV of 7.5° with an independent stabilised vertical movement of -15°/+60° and independent stabilised horizontal movement of 180° with a moving stabilisation accuracy of 0.05 mils in azimuth and elevation and minimum/maximum stabilised sight movements of 0.03/60 deg/s with an angular tracking rate of 60 deg/s with FLIR enabling a max range of 30 km, detection of tank sized targets up to 12 km and identification up to 3 km with detection of corvette sized warships up to 28 km with identification up to 20 km with detection of fighter sized targets up to 20 km and identification up to 4 km with an automatic target tracking range up to 8 km, TV sight enabling a max range of 20 km, detection of tank sized targets up to 13 km and identification up to 10 km with detection of fighter sized targets up to 16 km and identification up to 14 km with NFOV detection of corvette sized warships up to 18 km with identification up to 15 km with identification up to 25 km, IRST with automatic target tracking, automatic target slaving and automatic target recognition with tracking of 4 targets with an Angular resolution of 0.05° and max tracking rate of 200 deg/s enabling a max range up to 180 km with a 120 to 150 km detection range and 70 to 90 km rear track range with 35 km front track range and a 60 km track range for ground targets and laser targeting with laser rangefinding, laser designation and laser spot tracking with an accuracy of 5m with a 20 km engagement range for aircraft and 30 km engagement range for ground targets. NSTsI-KOS HMD with a 170° horizontal FOV and -35°/+85° vertical FOV with a target engagement range up to 20 km) 


Counter Measures: L-006M/SPO-15LM Beryoza-LM 2nd Generation digital RHAWS with 8 targets tracked with 6 preprogrammed threat identifiers and 5× receivers enabling a self protection envelope of 360° in azimuth and ±60° in elevation with band coverage of 4.4-10.3 GHz with a signal detectability range up to 225 km. SSP-2I digital fire countermeasure system. K-36DM Zero-Zero ejection seat. APP-50 countermeasure dispenser utilising 1st Generation IRCM and RFCM with 192 total rounds using the PPR-50 composite aluminium chaff that activates in 0.3 seconds and creates a false target RCS of greater than 60m² and using the PPI-50 thermite based flare with a minimum burn time of 3 seconds. SO-69/SRZO-2P 2nd Generation solid state IFF interrogator / transponder linked to the Parol fully digital IFF system with aircraft ID, full digital data encryption, reprogramming and cryptographic encoding. P-591 digital ICAS. KKO-15LP digital full ECLSS. 


(K/M model adds L-150/SPO-32 Pastel 3rd Generation fully digital RHAWS with 16 targets tracked and 128> preprogrammed threat identifiers with guidance of up to 6 ARMs with 2 fired simultaneous and 10× receivers enabling a self protection envelope of 360° in azimuth and ±60° in elevation with band coverage of 1.2-18 GHz with a signal detectability range up to 320 km. SSP-2I digital fire countermeasure system. K-36DM Zero-Zero ejection seat. APP-50 countermeasure dispenser utilising 1st Generation IRCM and RFCM with 192 total rounds using the PPR-50 composite aluminium chaff that activates in 0.3 seconds and creates a false target RCS of greater than 60m² and using the PPI-50 thermite based flare with a minimum burn time of 3 seconds. SO-72/SRZO-2P 2nd Generation digital IFF interrogator / transponder linked to the Parol-2D fully digital IFF system with aircraft ID, full digital data encryption, radio/inertial navigation locating, reprogramming and cryptographic encoding. P-591 digital ICAS. KKO-15LP digital full ECLSS)


(SM adds L-150NU-30/SPO-32M Pastel-M 4th Generation fully digital data fused RHAWS with 20 targets tracked with 242> preprogrammed threat identifiers with guidance of up to 8 ARMs with 4 fired simultaneous with 16× receivers enabling a self protection envelope of 360° in azimuth and ±180° in elevation with band coverage of 0.2-20 GHz with a signal detectability range up to 440 km. K-36DM Zero-Zero ejection seats. SO-96/SRZ-035M 3rd Generation fully digital IFF interrogator / transponder linked to the Parol-2D fully digital IFF system with aircraft ID, full digital data encryption, radio/inertial navigation locating, reprogramming and cryptographic encoding. Digital ICAS. KKO-15LP digital full ECLSS. APP-50M countermeasure dispenser utilising 2nd Generation IRCM and RFCM with 192 total rounds using the PPR-50-17 composite aluminium jammer assisted chaff that activates in 0.3 seconds and creates a false target RCS of greater than 60m² and using the PPI-50-3 spectral flare with a minimum burn time of 3 seconds)


(From early 2020s onwards Parol-2D is replaced by Password-3 fully digital IFF system with aircraft ID, low observability data sharing, satellite navigation locating, full digital data encryption, reprogramming and cryptographic encoding)


(SM2 models add L-150-35/SPO-32M Pastel-M 4th Generation fully digital data fused RHAWS with 20 targets tracked with 242> preprogrammed threat identifiers with guidance of up to 8 ARMs with 4 fired simultaneous with 16× receivers enabling a self protection envelope of 360° in azimuth and ±180° in elevation with band coverage of 0.2-20 GHz with a signal detectability range up to 440 km. Type 4283MP/Type 4280MD fully digital low observability IFF interrogator/transponder linked to the Password-3 fully digital IFF system with low observability data sharing, satellite navigation locating, full digital data encryption, reprogramming and cryptographic encoding. SOZhE-35 fully digital ICAS, full ECLSS and fire countermeasure system. K-36D-5 Zero-Zero ejection seat. Blesna Diamant-S 3rd Generation RFCM with a towed decoy SPJ with a 100m towing range utilising simultaneous LPIR, monopulse, continuous wave and pulse doppler countermeasure. UV-50 countermeasure dispensers utilising 2nd Generation IRCM and 3rd Generation RFCM with 84 total rounds using PPR-50-17-110V composite aluminium jammer assisted chaff that activates in 0.3 seconds and creates a false target RCS of greater than 60m², PPI-50-3 spectral flare with a minimum burn time of 3 seconds and Lobushka disposable DRFM jammers with a jamming time up to 6 seconds)


Electronic Warfare: L-005S Sorbitsya-S 3rd Generation digital SPJ with monopulse countermeasure, continuous wave countermeasure and pulse doppler countermeasure ECCM with track breaker, track breaking and blip enhancement ELINT with 4× receivers enabling an ECCM protection envelope of 360° in azimuth with a self protection jamming range of 200 km> with SPS-171 3rd Generation digital active jamming system operating on 6-10 GHz with deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, cross eye jamming and spot jamming jamming ECM with 4× PESA pyramidal horn antenna ECM transmitters enabling an active jamming range of 200 km>. 


(SM model adds L-175U Khibiny-U 4th Generation fully digital SPJ utilising radio direction finder with AoA and PRF determination, simultaneous monopulse countermeasure, continuous wave countermeasure, pulse doppler countermeasure and LPIR countermeasure with doppler shifting, home on jam and anti burn though ECCM with track breaker, advanced decoy generation, blip enhancement and global navigation spoofing ELINT with 8× receivers enabling a passive ECCM protection envelope of 360° in azimuth with a self protection jamming range of 300 km> with SAP-518 4th Generation fully digital active jamming system operating on 5-18 GHz with frequency agile deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, cross eye jamming, spot jamming, wave jamming, power managed jamming and DRFM jamming ECM with 4× GaAs AESA pyramidal horn ECM transmitters enabling an active jamming range of 300 km>) 


(SM2 models add L-265M10-35 Khibiny-M 5th Generation fully digital ECM System with an SPJ suite utilising radio direction finder with AoA and PRF determination, simultaneous monopulse countermeasure, continuous wave countermeasure, pulse doppler countermeasure and LPIR countermeasure with doppler shifting, noise cloaking, home on jam, anti burn though and self jam resistance ECCM with track breaker, advanced decoy generation, blip enhancement, satellite interception and global navigation spoofing ELINT with 8× receivers enabling a passive ECCM protection envelope of 360° in azimuth with a self protection jamming range of 400 km> with SAP-518SM 5th Generation fully digital active jamming system operating on 2-20 GHz with frequency agile deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, interrupted jamming, cross eye jamming, spot jamming, wave jamming, power managed jamming and DRFM/ISRJ jamming ECM with 4× GaN AESA pyramidal horn antenna array ECM transmitters enabling an active jamming range of 400 km>)


Guns: GSh-30-1 30mm autocannon slaved to laser rangefinder and radar with an effective firing range up to 2 km. 


Ordinance Capacity: 10× hardpoints with max 4400 kg munition capacity and 150 rounds for guns


(K and M model adds 12× hardpoints with max 8000 kg munition capacity and 150 rounds for guns)


(SM models add 12× hardpoints with a max 10,000 kg munition capacity and 150 rounds for guns)


Weapons Systems 


Common Air to Air Payloads 

● 8× APU-470 racks with R-27R 2× APU-73 racks with R-73

● 8× APU-470 racks with 6x R-27R and 2x R-27T 2× SPS-171  

● 6× APU-470 racks with R-27R 2× APU-73 racks with R-73 2× SPS-171  


R-27R

3rd Generation Radar Missile 

9B-1101 Inverse Monopulse X band Semi Active Seeker with a digital phase comparison antenna array with an INS utilising a radio correction data link with back up inertial operting guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a radio proximity fuse and back up impact detonation with a continuous rod warhead enabling a blast radius of 10-15 m²

~90 km max Range at 10 km+ altitude 

~70 km max Range at 5 km+ altitude 

~50 km max Range at sea level 

~30 km engagement range vs RCS of 5m² at sea level 

~50 km engagement range vs RCS of 5m² at 5 km+ altitude 

~70 km engagement range vs RCS of 5m² at 10 km+ altitude 

~10 km NEZ range vs RCS of 5m² at sea level 

~20 km NEZ range vs RCS of 5m² at 5 km> altitude

~30 km NEZ range vs RCS of 5m² at 10 km> altitude

~Mach 4 at 5 km+ altitude 

~Mach 2 at sea level 

~Targeting Angles 35°

~Turn Rate 20 to 50 Deg/s

~Initial Acceleration of 210-370 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 74g 


R-27T 

4th Generation IR Missile 

Geofizika-36T LN² Cooled digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~70 km max Range at altitude 

~40 km max Range at sea level 

~60 km engagement range 

~All aspect lock range 5 km

~Rear aspect lock range 20 km

~Mach 4 at high altitude 

~Mach 2 at sea level 

~Rectile Speed: 125 Hz

~Flare rejection 0.6

~Gimbal limit: 55°

~Angular Tracking: 60 deg/s 

~Turn Rate 20 to 50 Deg/s

~Initial Acceleration of 210-370 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 74g 



R-73

4th Generation IR Missile 

Mayak-80 LN² Cooled digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~30 km max Range at 5 km> altitude 

~20 km max Range at sea level 

~20 km engagement range at 5 km>

~All aspect lock range 4 km

~Rear aspect lock range 10 km 

~Rectile Speed: 150 Hz

~Mach 3 at high altitude 

~Mach 2 at sea level 

~Flare rejection 0.6

~Gimbal limit: 45°

~Angular Tracking: 60 deg/s 

~Turn Rate 90 to 120 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 60g 



GSh-30-1

9A-4071K 30×165mm SAPHEI


K and M models adds 


Common Air to Air Payloads 

● 8× AKU-170 racks with R-77 2× APU-73 racks with R-74 2× SAP-518 

● 6× APU-470 racks with R-27ER 4× AKU-170 racks with R-77 2× APU-73 racks with R-74 


R-77

4th Generation Radar Missile 

9P-1348 Inverse Monopulse X band Active Seeker with a digital slotted planar antenna array with an INS utilising a radio correction data link with back up inertial operting guidance, home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a Z23nA radio proximity fuse and back up impact detonation with with a high explosive blast warhead enabling a blast radius of 10-15 m²

~150 km max Range at 10 km+ altitude 

~120 km max Range at 5 km+ altitude 

~58 km max Range at sea level 

~35 km engagement range vs RCS of 5m² at sea level 

~80 km engagement range vs RCS of 5m² at 5 km+ altitude 

~110 km engagement range vs RCS of 5m² at 10 km+ altitude 

~15 km NEZ range vs RCS of 5m² at sea level 

~25 km NEZ range vs RCS of 5m² at 5 km> altitude

~30 km NEZ range vs RCS of 5m² at 10 km> altitude

~8 km ARH lock range vs RCS of 1m²

~14 km ARH lock range vs RCS of 5m²

~22 km ARH lock range vs RCS of 10m²

~0.1 m² minimum target RCS for ARH lock 

~Mach 4 at high altitude 

~Mach 3 at sea level 

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~50g Overload Tolerance 

~8g launch limiter

~12g target limiter 


R-27ER

3rd Generation Radar Missile 

9B-1101E Inverse Monopulse X band Semi Active Seeker with a fully digital phase comparison antenna array with an INS utilising a radio correction data link with back up inertial operting guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a radio proximity fuse and back up impact detonation with a continuous rod warhead enabling a blast radius of 10-15 m²

~130 km max Range at 10 km+ altitude 

~110 km max Range at 5 km+ altitude 

~90 km max Range at sea level 

~70 km engagement range vs RCS of 5m² at sea level 

~90 km engagement range vs RCS of 5m² at 5 km+ altitude 

~110 km engagement range vs RCS of 5m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 5m² at sea level 

~30 km NEZ range vs RCS of 5m² at 5 km> altitude

~50 km NEZ range vs RCS of 5m² at 10 km> altitude

~Mach 5 at 10 km+ altitude 

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Targeting Angles 35°

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~60g Overload Tolerance 

~8g launch limiter 

~10g target limiter 


R-27ET 

4th Generation IR Missile 

Geofizika-36TE LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~120 km max Range at altitude 

~40 km max Range at sea level 

~80 km engagement range 

~All aspect lock range 20 km

~Rear aspect lock range 30 km

~Mach 4 at 10 km+ altitude 

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Rectile Speed: 125 Hz

~Flare rejection 0.6

~Gimbal limit: 55°

~Angular Tracking: 60 deg/s 

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 60g 



R-74

4th Generation IR Missile 

Mayak-80B LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~30 km max Range at 5 km> altitude 

~20 km max Range at sea level 

~20 km engagement range at 5 km>

~All aspect lock range 6 km

~Rear aspect lock range 10 km

~Mach 3 at 5 km> altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.6

~Gimbal limit: 60°

~Angular Tracking: 60 deg/s 

~Turn Rate 90 to 120 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 60g 


Laser Guided Bombs 

KAB-1500L 1st Generation LG HE  

KAB-1500L-Pr-E 2nd Gen Bunker Buster 

KAB-1500L-F-E 1st Generation FRAG-HE 

KAB-1500L-OD-E 1st Generation FAE 

KAB-1500L-K-E 1st Generation Cluster Bomb 

KAB-500L 1st Generation LG HE  

KAB-500L-Pr-E 2nd Gen Bunker Buster 

KAB-500L-F-E 1st Generation FRAG-HE 

KAB-500L-OD-E 1st Generation FAE 

KAB-500L-K-E 1st Generation Cluster Bomb 


Optically Guided Bombs 

KAB-1500Kr-Pr-E 2nd Gen Bunker buster 

KAB-1500Kr-F-E 2nd Generation FRAG-HE 

KAB-1500Kr-OD-E 2nd Generation FAE 

KAB-1500TK 2nd Generation MITL HE 

KAB-1500Kr 2nd Generation HE

KAB-500Kr 2nd Generation HE

KAB-500Kr-Pr-E 2nd Gen Bunker Buster 

KAB-500Kr-F-E 2nd Generation FRAG-HE 

KAB-500Kr-OD-E 2nd Generation FAE 

KAB-500Kr-K-E 2nd Generation Cluster Bomb


Land Attack Missiles 

Kh-25ML-M 2nd Generation Laser Guided HE 

Kh-25ML-F 2nd Gen Laser Guided FRAG-HE 

Kh-25MT-M 2nd Generation OG HE 

Kh-25MT-F 2nd Generation OG FRAG-HE 

Kh-25MTP-M 2nd Generation OG/IIR HE 

Kh-25MTP-F 2nd Generation OG/IIR FRAG-HE 

Kh-59-M 3rd Generation HE Cruise Missile

Kh-59-K 3rd Generation HEAT Cruise Missile

Kh-59-KE 3rd Gen Cluster Cruise Missile

Kh-59L-M 2nd Gen Laser Guided HE

Kh-59L-K 2nd Gen Laser Guided HEAT

Kh-59L-KE 2nd Gen Laser Guided Cluster 

Kh-59T-M 2nd Generation OG HE

Kh-59T-K 2nd Generation OG HEAT

Kh-59T-KE 2nd Generation OG Cluster 

Kh-29T-M 2nd Generation OG HE

Kh-29T-K 2nd Generation OG HEAT 

Kh-29L-M 2nd Generation Laser Guided HE 

Kh-29L-K 2nd Generation Laser Guided HEAT 

Kh-31A 3rd Generation Anti Ship 

Kh-31P 2nd Generation Anti Radiation 

Kh-58 2nd Generation Anti Radiation  


Unguided Bombs 

FAB-500 HE bomb

FAB-250  HE bomb

BETAB-500 bunker buster

RBK-500 cluster munition bomb

RBK-250 cluster munition bomb

KMGU cluster munition dispenser 


Rockets

S-24 HE-FRAG Rocket


B-13L Rocket Pod

S-5M HE-FRAG Rocket 

S-5K HEAT Rocket 

S-5S Flechette Rocket 


B-8M1 Rocket Pod

S-8S Flechette rocket 

S-8P chaff rocket 

S-8D FAE rocket 

S-8KO HEAT Rocket 

S-8B Bunker buster rocket 


UB-32 Rocket Pod 

S-13 KEP Rocket 

S-13T HEAT Rocket 



Weapons Systems for SM


Common Air to Air Payloads 

● 4× AKU-170M dual racks with R-77-1 4× AKU-170 racks with R-77-1 2× APU-73 racks with R-74M 2× SAP-518 wing pods

● 4× AKU-170M dual racks with R-77-1 6× AKU-170 racks with R-77-1 2× APU-73 racks with R-74M 


Common Air to Ground Payloads 

2x O-25 2x B-13L 2x R-74M 2× SAP-518

4x Kh-31AD 2x Kh-35U 1x Kh-61 2x R-74M 2× SAP-518

4x Kh-58U 2x Kh-31PD 2x R-74M 2× SAP-518

4x Kh-29D 4x Kh-29ML 2x R-74M 2× SAP-518

4x Kh-59M2 4x KAB-500OD 2x R-74M 2× SAP-518

2x KAB-1500Kr-OD 4x Kh-29D 2x R-74M 2× SAP-518

2x Kh-59MKM 2x Kh-69 2x KAB-1500LG-Pr-E 

2x R-74M 2× SAP-518



R-77-1B

4+ Generation Radar Missile 

9B-1103M-150 Inverse Monopulse X/Ku band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a bi-directional radio correction data link with back up inertial operting guidance, dual band, home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser and Z23nA radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~200 km max Range at 10 km+ altitude 

~150 km max Range at 5 km+ altitude 

~80 km max Range at sea level 

~50 km engagement range vs RCS of 5m² at sea level 

~110 km engagement range vs RCS of 5m² at 5 km+ altitude 

~140 km engagement range vs RCS of 5m² at 10 km+ altitude 

~30 km NEZ range vs RCS of 5m² at sea level 

~40 km NEZ range vs RCS of 5m² at 5 km> altitude

~60 km NEZ range vs RCS of 5m² at 10 km> altitude

~8 km ARH lock range vs RCS of 1m²

~20 km ARH lock range vs RCS of 5m²

~26 km ARH lock range vs RCS of 10m²

~0.05 m² minimum target RCS for ARH lock 

~Mach 5 max target velocity 

~Mach 4 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~Launch limiter 9g 

~Target limiter 12g 

~Overload Tolerance 60g


R-27ET 

4th Generation IR Missile 

Geofizika-36TE LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~120 km max Range at altitude 

~40 km max Range at sea level 

~80 km engagement range 

~All aspect lock range 20 km

~Rear aspect lock range 30 km

~Angular tracking 60 deg/s

~Mach 4 at 10 km+ altitude 

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Rectile Speed: 125 Hz

~Flare rejection 0.6

~Gimbal limit: 55°

~Angular Tracking: 60 deg/s 

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 60g 


R-74M

4+ Generation IR Missile 

Impuls-90 LN² Cooled NIR & UV channel fully digital pseudo-imaging HgCdTe Seeker with dual band, gatewidth and seeker shut off IRCCM

~50 km max Range at 5 km> altitude 

~40 km max Range at sea level 

~40 km engagement range at 5 km> altitude

~All aspect lock range 10 km

~Rear aspect lock range 10 km 

~Mach 3 at 5 km> altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.8

~Gimbal limit: 75°

~Angular Tracking: 60 deg/s 

~Turn Rate 120 to 180 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 80g 


Air to Ground Missiles  

Kh-69 LO 4th Gen Cluster Cruise Missile 

Kh-69 LO 4th Gen HEAT Cruise Missile 

Kh-59MK2-F-E LO 3rd Gen OG/IIR FRAG-HE 

Kh-59M2-M 2nd Generation OG HE 

Kh-59M2-K 2nd Generation OG HEAT 

Kh-59M2-KE 2nd Generation OG Cluster 

Kh-59M2D-M 2nd Generation OG/IIR HE 

Kh-59M2D-K 2nd Generation OG/IIR HEAT 

Kh-59M2D-KE 2nd Generation OG/IIR Cluster 

Kh-59MK-M 4th Generation HE Cruise Missile

Kh-59MK-K 4th Gen HEAT Cruise Missile

Kh-59MK-KE 4th Gen Cluster Cruise Missile

Kh-58UShKE 3rd Gen Anti Radiation  

Kh-58UShKE-TP 3rd Gen OG/IIR Anti Radiation

Kh-29MP-M 4th Gen HE Ballistic Missile 

Kh-29MP-K 4th Gen HEAT Ballistic Missile 

Kh-29TE-M 3rd Generation OG HE 

Kh-29TE-K 3rd Generation OG HEAT 

Kh-29TD-M 3rd Generation OG/IIR HE 

Kh-29TD-K 3rd Generation OG/IIR HEAT 

Kh-29ML-M 3rd Generation Laser Guided HE 

Kh-29ML-K 3rd Gen Laser Guided HEAT   


Bunker Busters 

Kh-59MKM 3rd Generation Bunker Buster 

Kh-59MK2-Pr LO 3rd Gen Bunker Buster 

KAB-500Kr-Pr-E 2nd Gen Bunker Buster 

KAB-500LG-Pr-E 2nd Gen Bunker Buster

KAB-250LG-Pr-E 2nd Generation Bunker Buster

BETAB-500SHP 1st Generation bunker buster

BETAB-500 1st Generation Bunker buster 

BETAB-500Y 1st Generation Bunker buster 


Laser Guided Bombs 

KAB-20LG-K 3rd Generation HEAT 

KAB-20LG-FE 3rd Generation FRAG-HE  

KAB-50LG-K 3rd Generation HEAT 

KAB-50LG-FE 3rd Generation FRAG-HE  

KAB-100LG-K 3rd Generation HEAT 

KAB-100LG-FE 3rd Generation FRAG-HE 

KAB-250LG 3rd Generation HE 

KAB-250LG-F-E 3rd Generation FRAG-HE 

KAB-250LG-OD-E 3rd Generation FAE

KAB-500MLG 3rd Generation HE

KAB-500MLG-Pr-E 3rd Gen Bunker Buster 

KAB-500MLG-F-E 3rd Generation FRAG-HE 

KAB-500MLG-OD-E 3rd Generation FAE 

KAB-500MLG-K-E 3rd Gen Cluster Bomb


Optically Guided Bombs 

KAB-50Kr-M-K 3rd Generation HEAT 

KAB-50Kr-MT-K 3rd Generation IIR HEAT 

KAB-50Kr-M-FE 3rd Generation FRAG-HE 

KAB-50Kr-MT-FE 3rd Generation IIR FRAG-HE 

KAB-250Kr-M 3rd Generation HE 

KAB-250Kr-M-F-E 3rd Generation FRAG-HE 

KAB-250Kr-M-OD-E 3rd Generation FAE

KAB-500Kr-M 3rd Generation HE

KAB-500Kr-M-Pr-E 3rd Gen Bunker Buster 

KAB-500Kr-M-F-E 3rd Generation FRAG-HE 

KAB-500Kr-M-OD-E 3rd Generation FAE 

KAB-500Kr-M-K-E 3rd Gen Cluster Bomb


Satellite Guided Munitions 

Kh-25MS-M Satellite guided HE 

Kh-25MS-F Satellite guided FRAG-HE 

KAB-250S-E satellite guided HE bomb 

KAB-500S-E Satellite guided HE bomb 

KAB-500Kr UMPK Satellite guided TV bomb 

ZAB-100 UMPK satellite guided Incen bomb 

ZAB-250 UMPK satellite guided Incen bomb

ODAB-500 UMPK satellite guided FAE bomb 

RBK-500 UMPK satellite guided cluster bomb

FAB-250 UMPK satellite guided HE bomb 

FAB-500 UMPK satellite guided HE bomb 

FAB-250 UMPB satellite guided HE bomb 

FAB-500 UMPB satellite guided HE bomb 


Unguided Bombs 

FAB-250 Unguided HE Bomb 

FAB-500 Unguided HE Bomb 

OFAB-150 Unguided Frag Bomb 

OFAB-250 Unguided Frag Bomb 

OFAB-500 Unguided Frag Bomb 

PLAB-250-120 Unguided ASW bomb 

ZAB-100-105 Unguided Incendiary bomb

ZAB-250-200 Unguided Incendiary bomb 

ODAB-500 Unguided fuel air bomb 

PTAB-500 Unguided anti tank bomb 

PTAB-500Y Unguided Anti Tank bomb 


Rockets 

S-25L 2nd Generation laser guided rocket

S-25-OFM 1st Generation Bunker buster 

S-25-OF high explosive Rocket 

S-13B 1st Generation Bunker buster 

S-13T tandem HEAT AT round 

S-13OF AP Anti armour frag round 

S-13DF thermobaric round 

S-13Kor 2nd Generation laser guided rocket


GSh-30-1 

9-A1-4071K 30x165mm HEI

9-A1-4071K 30x165mm HE-T

9-A1-4071K 30x165mm AP-T

9-A1-4071K 30x165mm SAPHEI

9-A1-4071K 30x165mm MKETF


Cluster Munitions

KMGU-2 cluster Munition dispenser 


Later models add 


R-77-1C

4+ Generation Radar Missile 

9B-1103M-200PA Inverse Monopulse Ku band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a bi-directional radio correction data link with back up inertial operting guidance, home on jam, multimode guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser and Z23nA radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~200 km max Range at 10 km+ altitude 

~150 km max Range at 5 km+ altitude 

~80 km max Range at sea level 

~50 km engagement range vs RCS of 3m² at sea level 

~100 km engagement range vs RCS of 3m² at 5 km+ altitude 

~120 km engagement range vs RCS of 3m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 3m² at sea level 

~40 km NEZ range vs RCS of 3m² at 5 km> altitude

~60 km NEZ range vs RCS of 3m² at 10 km> altitude

~10 km ARH lock range vs RCS of 1m²

~20 km ARH lock range vs RCS of 3m²

~30 km ARH lock range vs RCS of 10m²

~0.05 m² minimum target RCS for ARH lock 

~Mach 5 max target velocity 

~Mach 4 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~Launch limiter 9g 

~Target limiter 12g 

~Overload Tolerance 60g



SM2 model adds 

● 8× AKU-170 racks with R-77M 2× APU-73 racks with R-74M2 2× SAP-518SM

● 4× AKU-620 racks with R-37M 4× AKU-170 racks with R-77M 2× APU-73 with R-74M2 2× SAP-518SM wing pods 

● 4× AKU-170M dual racks with R-77M 4× AKU-170 racks with R-77M 2× APU-73 racks with R-74M2 2× SAP-518SM wing pods

● 4× AKU-170M dual racks with R-77M 6× AKU-170 racks with R-77M 2× APU-73 racks with R-74M2


R-77M

5th Generation Radar Missile 

9B-1103M2 Ka/Ku band AESA Active Seeker with 64 GaAs T/R modules using an fully digital patch antenna array with an INS/GNSS utilising a bi-directional radio correction data link with back up inertial operting guidance, LPIR, home on jam, dual band seeker and polarisation filtering ECCM utilising a solid fuel dual pulse rocket motor with a laser and radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~300 km max Range at 10 km+ 

~250 km max Range at 5 km+

~150 km max Range at sea level 

~120 km engagement range vs RCS of 1m² at sea level 

~190 km engagement range vs RCS of 1m² at 5 km+ altitude 

~220 km engagement range vs RCS of 1m² at 10 km+ altitude 

~50 km NEZ range vs RCS of 1m² at sea level 

~70 km NEZ range vs RCS of 1m² at 5 km> altitude

~90 km NEZ range vs RCS of 1m² at 10 km> altitude

~2 km ARH lock range vs RCS of 0.003m²

~14 km ARH lock range vs RCS of 1m²

~26 km ARH lock range vs RCS of 3m²

~35 km ARH lock range vs RCS of 10m²

~0.0005 m² minimum target RCS for ARH lock 

~Mach 6 max target velocity 

~Mach 5 top speed above 5 km altitude 

~Mach 3 top speed at sea level

~Targeting Angles 60°

~Turn Rate 70 to 120 Deg/s

~Initial Acceleration of 300-600 m/s>

~Launch limiter 10g 

~Target limiter 12g 

~Overload Tolerance 80g


R-37M

4+ Generation Radar Missile 

9B-1103M-350 Inverse Monopulse Ku/X band Active Seeker with an fully digital slotted planar antenna array with an INS/GNSS utilising a bi-directional radio correction data link with back up inertial operting guidance, home on jam, dual band seeker and polarisation filtering ECCM utilising a solid fuel dual pulse rocket motor with a kolibri radio proximity fuse with back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-20 m²

~400 km max range at 10 km+ altitude 

~300 km max Range at 5 km+ altitude 

~150 km max Range at sea level 

~120 km engagement range vs RCS of 3m² at sea level 

~200 km engagement range vs RCS of 3m² at 5 km+ altitude 

~300 km engagement range vs RCS of 3m² at 10 km+ altitude 

~70 km NEZ range vs RCS of 3m² at sea level 

~90 km NEZ range vs RCS of 3m² at 5 km> altitude

~120 km NEZ range vs RCS of 3m² at 10 km> altitude

~20 km ARH lock range vs RCS of 1m²

~40 km ARH lock range vs RCS of 3m²

~70 km ARH lock range vs RCS of 10m²

~0.005 m² minimum target RCS for ARH lock 

~Targeting Angles 45°

~Turn Rate 10 to 60 Deg/s

~Initial Acceleration of 600-900 m/s>

~8g launch limiter

~8g target limiter 

~40g overload tolerance 

~Mach 6 max target velocity 

~Mach 6 top speed above 5 km altitude 

~Mach 4 top speed at sea level


R-74M2

5th Generation IR Missile 

Karfagen-760 LN² Cooled MIR & UV channel fully digital pseudo-imaging HgCdTe LOAL Seeker with dual band, MITL, IOG, gatewidth and seeker shut off IRCCM

~60 km max Range 

~50 km range at sea level 

~50 km engagement range 

~All aspect lock range 10 km

~Rear aspect lock range 10 km

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Flare rejection 0.9+

~Turn Rate 120 to 180 Deg/s

~Initial Acceleration of 300-400 m/s>

~Rectile Speed: 200 Hz

~Gimbal limit: 180°

~Angular Tracking: 75 deg/s 

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 80g

Su-30 

Su-30K

Su-30M 

Su-30SM


Su-30SM2 

Su-30MKI 
Su-30MKM 
Su-30MKA
Su-30MKK 








Su-27 Flanker Series 

Su-27S

Concept: 1969

Designed: 1970

Prototype: 1977

Completed: 1984

Production: 1985

Service: 1990

Generation: 4th

Aircraft Role: Air Superiority 

Combat Rank: S

Number Made: 1000+


Su-27SM 

Prototype: 2002

Production: 2004

Service: 2006

Generation: 4+

Aircraft Role: MultiRole/Air Superiority 

Number Made: 100+


Su-27SM3 

Prototype: 2008

Production: 2009

Service: 2011

Generation: 4+

Aircraft Role: MultiRole/Air Superiority 

Number Made: 20+


Su-27K

Designed: 1984

Prototype: 1987

Completed: 1990

Production: 1992 

Service: 1994

Generation: 4th

Aircraft Role: Air Superiority 

Combat Rank: D

Number Made: 20+


Su-27KUB

Designed: 1997

Prototype: 1999

Generation: 4th

Aircraft Role: Air Superiority 

Combat Rank: D

Number Made: 3


Su-33

Designed: 1994

Prototype: 1999

Completed: 2000

Production: 2002 

Service: 2004

Generation: 4th

Aircraft Role: Air Superiority 

Combat Rank: D

Number Made: 14


Su-33M

Designed: 1999

Prototype: 2011

Completed: 2013

Production: 2015

Service: 2018

Generation: 4th

Aircraft Role: MultiRole/Strike Fighter 

Combat Rank: D

Number Made: 14


Engine and Airframe: All metal construction with an RCS minimum of 10m². Crew of 1. Length: 22 m. Height: 6 m. Wingspan 14.7 m. Wing area: 62 m². Frame weight 16,380 kg. Takeoff weight: 33,000 kg. Max Fuel: 9,400 kg. 2× Lyul'ka-Saturn AL-31F axial flow low bypass turbofans with an analogue electronic engine control with 156 kN of thrust and 246 kN in afterburner. 


(SM3 model adds 2× Lyul'ka-Saturn AL-31-FM1 axial flow low bypass turbofans with a digital electronic engine control) 


Speed and Endurance: Top speed of mach 2.2 to 2.5 at 15 km+, mach 2 to 2.2 at 10 km+, mach 1.8 to 2 to at 5 km+ and mach 1 to 1.3 at sea level. Service Ceiling of 20 to 23 km. Combat range of 1200-1500 km. Acceleration 9-18 seconds to mach 1 sea level. Stall speed 170-220 kph. Take off distance is 600m with ATA payload to 1300m for full payload. Landing distance 900 to 1100m. In flight refueling. 


Manuvarabilities: Thrust to weight ratio of 1 at full air to air payload and 1.3 at half fuel/loadout and 0.9 at full loadout. Roll rate of 180 deg/s at high speed and 270 deg/s at low speed. Climb rate of 260-230 m/s. No AOA limit at low speeds with 59° angle of attack at mach 1>. 14 to 22 kph/s speed bleed at high g instantaneous maneuvers and 11 to 31 kph/s speed bleed at high g sustained maneuvers. Wing loading of 370-410 kg/m². Sustained G tolerance of 9g with a max Overload Tolerance of 13g and wing break at 19.5g. 4× LERXs with pitch of ±40° and 2× elevators with pitch of -30°.


Aircraft Turn Rates 


Sustained turn rates 


Mach ~1.5 Speeds 

● 1 deg/s at 10 km altitude 

● 1-3 deg/s at 5 km altitude 

● 3-6 deg/s at sea level   


Mach ~1 Speeds 

● 9-10 deg/s at 10 km altitude 

● 11-13 deg/s at 5 km altitude 

● 14-17 deg/s at sea level   


Mach ~0.5 Speeds 

● 12-14 deg/s at 10 km altitude 

● 13-16 deg/s at 5 km altitude 

● 16-20 deg/s at sea level   


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 3-4 deg/s at 10 km altitude 

● 6-8 deg/s at 5 km altitude 

● 9-12 deg/s at sea level    


Mach ~1 Speeds 

● 12-16 deg/s at 10 km altitude 

● 13-22 deg/s at 5 km altitude 

● 16-28 deg/s at sea level    


Mach ~0.5 Speeds 

● 19-22 deg/s at 10 km altitude 

● 22-26 deg/s at 5 km altitude 

● 25-30 deg/s at sea level    


Airframe RCS

RCS Minimum: 10m²

RCS Median: 12m²

RCS Average: 15-20m²


Navigation & Flight Control: PrNK-10 computerised navigation suite with a SAU-10 3× axis computerised autopilot and an SDU-10 analogue fly by wire AFCS utilising a SVS-2Ts-2 4x bit digital ADC with a 50-100k SLOC-OS with navigation systems, electronic flight control and autopilot link. PNK-10-02 digital navigation system with a Ts-050 8x bit digital navigation computer using IP-1-72A/IS-1-72A digital INS with a digital tuning fork quartz and gyrostabilized accelerometer with an accuracy of 0.1° in pitch and yaw and 0.2° in heading with an error rate of 3.5 km/ph and velocity error rate of <3 m/s. SOI-10 2nd Generation cockpit with 1× CRT MFD and HOTAS control stick. RV-20 solid state radar altimeters. ARK-22 solid state ADF. RSDN-20 Alpha digital radio navigation system with DVOR and ILS with a position accuracy of 20-90m and angular accuracy of ±0.1°. ZSh-5 Flight Helmet. 


(SM models adds PrNK-27SM fully computerised navigation suite with a SAU-10SM 6× axis computerised autopilot and a SDU-27 digital fly by wire AFCS utilising a TsSVS-90 32x bit digital ADC with a PNK-11 fully digital navigation system utilising a Ts-061K 32x bit fully digital navigation computer using a fully digital INS utilising a ring laser gyroscope and gyrostabilized accelerometer with an accuracy of 0.04° in pitch and yaw and 0.07° in heading with an error rate of 1.3 km/ph and velocity error rate of <1 m/s with a hybridised position accuracy of <30m. RSBN-85 Vstrecha fully digital radio navigation system with DVOR and ILS with a position accuracy of 10-20m and angular accuracy of ±0.01°. MFI-10 4th Generation cockpit with 2× FHD LCD MFDs and HOTAS control stick. ZSh-7AP Flight Helmet. ARK-25 digital ADF. RV-21 digital radar altimeter. A-737 GLONASS-M Global navigation satellite system with a max CEP of 2m and average CEP of 10m. (When inside former USSR airspace SDCM GNSS augmentation improves precision with a max accuracy of 1m and average accuracy of <4m)


(SM3 adds MFI-10-2 4th Generation cockpit with 3× FHD LCD MFDs and HOTAS control stick)  


Fire Control: SUO-27 computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with digital sensors with stability augmentation with the OEPrNK-10 data fusion system utilising NAV, IFF, RDR, IDL and IRST information displayed on one screen with RLPK-27 radar targeting system and OEPS-27 laser and infrared tracking targeting system with a Ts-100 digital FCC utilising 580VM80 8x bit CPUs performing 170-200k IPS and 20-30m FLOPS. N001 Mech 3rd Generation X band mechanically steered solid state long chord twist cassegrain antenna array using analogue to digital signal processing, coherent doppler filtering based LDSD with pulse doppler IFF and tactical data link integration with CW illumination for SARH guidance, reduced false alarm rates, BIST system and computerised radar image displayed with multi-mode operation, predictive flight path and non tracked target tracking functions and raster, conical, sector, circular and spiral scan scanning modes utilising SRC/LDSD, STTR, MTTR and HMD, LDR, IRST and RFR based ACMs air to air radar modes with gain modulation, notch filtering, polarization filtering and pulse compression ECCM with HPRF power output on average being 1 kW with a 8 kW max output with 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance and 1 channel for sidelobe suppression and ECM with a noise factor of 6 dB with a 1074 mm antenna diameter. ILS-31 4th Generation HUD with a digital LED glass display utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with an integrated digital bombing complex utilising gun, bomb and rocket CCRP and CCIP with gun EEGS. IPV 4th Generation Radar display with an SVD system utilising a polychrome raster image displayed on a CRT MFD with computerised target generation, ECM resolution, navigation data and aircraft flight information with data link integration. ZSh-5 Helmet with Shchel-3UM 1st Generation HMD. OLS-27 2nd Generation IRST with a LN² cooled pseudoimaging InSb detector and 12P2-01 1.06 μm Nd:YAG laser rangefinder. TsVB-10 digital ballistic computer utilising a 580VM80 8x bit CPU enabling gun and missile coursing. 


(SM models add SUO-27ESh fully computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with fully digital sensors with full stability augmentation with utilising OEPrNK-27 data fusion system utilising IFF, NAV, RDR, IRST, EOT and TDL information displayed on one screen with the RLPK-27 radar targeting and OEPS-27SM electro optical, laser and infrared imaging/tracking targeting utilising a Baget-55-04.02 fully digital FCC with KOMDIV-32 32x bit CPUs performing 1-4b IPS and 10-15b FLOPS. OLS-30 multi-channel fully digital EOTS with a HD resolution TV sight with a ~720p day time image resolution, 1.06 μm Nd:YAG laser targeting system with laser rangefinding, laser designation and laser spot tracking and a 2nd Generation IRST & 2nd Generation FLIR system utilising a LN² cooled infrared imaging InSb detector with an FPA format of 96x4 and a thermal image resolution of 576×480p. N001VEP Mech-VEP 3++ Generation X band mechanically steered solid state long chord twist cassegrain antenna array using programmable analogue to digital signal processing, coherent doppler filtering based LDSD with and pulse doppler IFF and tactical & missile data link integration with CW illumination for SARH guidance, reduced false alarm rates, BIST system and computerised radar image displaying with multi-mode operation, predictive flight path and non tracked target tracking functions and raster, conical, sector, circular and spiral scan scanning modes utilising GTD, GTT and SAR air to ground radar modes and SRC/LDSD, STTR, MTTR and HMD, LDR, IRST, EOT and RFR based ACMs air to air radar modes with gain modulation, notch filtering, polarization filtering and pulse compression ECCM with the main antenna being 1074 mm diameter in size and HPRF power output on average being 1 kW with a 10 kW max output with 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance and 1 channel for sidelobe suppression and ECM with a noise factor of 6 dB. 5th Generation Radar display with an SVD system utilising a high resolution full colour raster image displayed on a LCD MFD with computerised target generation, ECM resolution, navigation data and aircraft flight information with data link integration. ZSH-7AP Flight Helmet with NSTs-T-04 1st Generation HMD utilising automatic cueing for targeting with head tracking software. TsVB-27SM digital ballistic computer utilising a KN1801VM3 16x bit CPU enabling automatic digital target lead and gun and missile coursing with gun, rocket and bomb CCRP and CCIP with a max bomb and rocket accuracy of <10-20m CEP at a range up to 2000m and altitudes up to 3000m and <100-300m CEP at a range up to 10,000m and altitude up to 10,000m)


(SM3 model adds Khibiny data fusion system with RFCM, IRCM, MAW, ESM, ECM and RHAWS information displayed on one screen) 

 

Communication & C2: K-DIAE digital unified communication complex with R-862/R-800 VHF/UHF and R-864 HF digital radios with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding and digital data encryption with text and voice formats utilised operating on 20 channels with data transfer speeds of 1.2 kbit/s, 10 kbit/s and 16 kbit/s with an operating communication range of 350 km with an integrated LChM FHSS system utilising up to 100 frequency hops per second and VChP CRNG encoding system with 10 round cryptographic encryption for 56 bit and 8 round cryptographic encryption for 96 bit and the TKS-2 digital information data link linked to the Voyska PVO NDCC air defence network with digital electronics, frequency hopping, ECM resistance, two way communication, digital data encryption, multi aircraft link, IFF integration, electronic countermeasure support and C2 integration utilising ground and air based computer and radar generated data exchange with pre recorded voice, text and image formats used, with data transfer speeds of 75 bit/s, 150 bit/s, 300 bit/s, 1200 bit/s, 2400 bit/s and 4800 bit/s every 2 to 10 seconds operating on 3 MHz to 300 MHz with up to 20,000 frequency hops per second on 26 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1000 km with data exchange between up to 16 aircraft. Rubezh-M digital GCI complex with the Spektr-1 and Biryusa digital navigation data links and BAN-75, SVPK, SPK-75 and SPK-68 digital command data links connected to the SAU-10 computerised autopilot, ARK-22 solid state ADF, SO-69 solid state IFF interrogator and SRZO-2P solid state IFF transponder linked to the PVO NDCC air defence network with fully automated ground controlled interception, weapons management, IFF integration, digital data encryption and navigation data utilising ground based computer and radar generated data exchange with pre recorded voice and text formats used with data transfer speeds of 45 bit/s, 80 bit/s and 96 bit/s every 5 to 10 seconds operating on 2 MHz to 400 MHz with up to 1000 frequency hops per second on 10 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1000 km with data exchange between up to 36 aircraft. 


(33, KUB and SK models added N001V Mech-V 3rd Generation X band mechanically steered solid state long chord twist cassegrain antenna array using analogue to digital signal processing, coherent doppler filtering based LDSD with and pulse doppler IFF and tactical & missile data link integration with CW illumination for SARH guidance, reduced false alarm rates and computerised radar image displaying with multi-mode operation, predictive flight path and non tracked target tracking functions and raster, conical, sector, circular and spiral scan scanning modes utilising SRC/LDSD, STTR, MTTR and HMD, LDR, IRST and RFR based ACMs air to air radar modes with gain modulation, polarization filtering and pulse compression ECCM with HPRF power output on average being 1-2 kW with a 8 kW max output with 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance and 1 channel for sidelobe suppression and ECM with a noise factor of 6 dB with a 1074 mm antenna diameter. with a Ts-101M digital FCC utilising K1801 16x bit CPUs performing 300-400k IPS and 150-200m FLOPS)


(SM models adds S-103 fully digital unified communication complex with an R-833 fully digital software defined VHF/UHF and HF radio with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding, rekeying encryption and full digital data encryption with text, image and voice formats utilised operating on 8 programmable channels and 256 frequency carriers with data transfer speeds of 16 kbit/s, 5 mbit/s and 11 mbit/s utilising an PPCh integrated FHSS and CRNG system utilising up to 1000 frequency hops per second and 7 round cryptographic encryption for 128 bit, 9 round cryptographic encryption for 192 bit and 10 round cryptographic encryption for 256 bit with an operating LOS communication range of 450 km and BLOS up to 5000 km with satellite link and the TCS-2M fully digital Tactical Data Link linked to NDMC NTsUO military command center utilising the YeESU-TZ military C4 network that organises coordination between the Voiska PVO-PRO air defence network and the PTK blue force tracking network with links to Andromeda-D, Akatsiya-E, Barnaul-T, Baikal-1ME, Universal-1E, Fundament-M and Polyana-D4M1 C2 softwares and Type-1B, Planet and VIP-117M3 data terminals with fully automated VOR, GCI and ILS with fully digital electronics, frequency hopping, ECM resistance, two way communication, navigation data, fully digital data encryption, multi aircraft link, multi platform subscription, weapons management, IFF integration, electronic countermeasure support and C4 integration utilising ground and air based computer and radar generated data exchange with pre recorded voice, text and image formats used, with data transfer speeds of 1024 bit/s, 1200 bit/s, 2.4 kbit/s, 4.8 kbit/s and 16 kbit/s every 1 to 2 seconds operating on 3 MHz to 300 MHz with up to 20,000 frequency hops per second on 26 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1500 km with data exchange between up to 20 subscribers. BTsVM-900 fully digital FMC utilising i486DX4-90 32x bit CPUs performing 2-3b IPS and 90-120b FLOPS using the RelMK32 1-2m SLOC RTOS using a BTsK-27 C2IS suite linked to the YeESU-TZ military C4 network with squads level blue force tracking, SATCOM integration, electronic countermeasure support, precision targeting, integrated aircraft health management software, digital navigation software, moving map display and data sharing) 


(33M add SVP-24 fully computerised radar, laser and electro optical targeting system. SV-24 fully digital ballistic computer with satellite aided targeting utilising a 32x bit CPU enabling fully automatic digital target lead with gun, rocket and bomb CCRP and CCIP with a max gun accuracy, whilst flying up to 700 kph, under 0.5 MRAD up to 4000m and under 0.1 MRAD up to 2000m and bomb and rocket accuracy of <3-5m CEP at a range up to 2000m and altitudes up to 5000m and <30-40m CEP at a range up to 10,000m and altitude up to 12,000m. KAI-24 5th Generation HUD with an integrated all digital bombing complex with gun, bomb and rocket CCRP and CCIP. OLS-30 multi-channel fully digital EOTS with a HD resolution TV sight with a ~720p day time image resolution, 1.06 μm Nd:YAG laser targeting system with laser rangefinding, laser designation and laser spot tracking and a 2nd Generation IRST & 2nd Generation FLIR system utilising a LN² cooled infrared imaging InSb detector with an FPA format of 96x4 and a thermal image resolution of 576×480p)


Targeting: Mech radar with 120° horizontal and -55°/+60° vertical scan range enabling tracking of up to 10 targets with an Rmax range up to 200 km, 140 km detection range for 16m² RCS and track range of 70 km for 3m² RCS with a LDSD detection range of 20-40 km for 16m² and a LDSD track range of 18-32 km for an aircraft with an RCS of 3m² with a rangefinding radar gun engagement range up to 10 km with a tracking scan range of 80° in azimuth and -15°/+25° in elevation and a tracking scan time of 5 seconds with max tracking target velocity at over 2500 kph and stores tracking information for up to 2 non tracked target with predictive flight paths for non tracked targets up to 10 seconds with LDSD ground clutter rejection of 60> dB and low chaff rejection with a MTBF of 5 to 60 hours. OLS-27 IRST with single target tracking and automatic target track with an angular resolution of 0.1° and max tracking rate of 30 deg/s enabling a max range up to 90 km with a 50 to 80 km detection range 20 to 30 km rear track range with 15 km front track range for fighter sized targets and laser targeting system with laser rangefinding with an accuracy of 10m and a 8 km engagement range for aircraft with a horizontal FOV up to 120° and a vertical FOV of -15°/+60°. Shchel-3UM HMD with a 120° horizontal FOV and ±30° vertical FOV up to 10 km.


(1990 models onwards and 33 added Mech-V radar with 120° horizontal and -55°/+60° vertical scan range enabling tracking of up to 10 targets and data linking of 2 missiles with a Rmax range up to 200 km, 140 km detection range for 16m² RCS and track range of 80 km for 3m² RCS with a LDSD detection range of 40-50 km for 16m² and a LDSD track range of 30-45 km for an aircraft with an RCS of 3m² with a rangefinding radar gun engagement range up to 10 km with a tracking scan range of 80° in azimuth and -15°/+25° in elevation and a tracking scan time of 5 seconds with max tracking target velocity at over 2500 kph and stores tracking information for up to 2 non tracked target with predictive flight paths for non tracked targets up to 10 seconds with LDSD ground clutter rejection of 60> dB and low chaff rejection with a MTBF of 60 to 100 hours)


(33M, SM, SM3 and KUB model adds Mech-VEP radar with a 120° primary horizontal and -55°/+60° vertical scan range enabling tracking of up to 12 targets and data linking of 4 missiles with Rmax range up to 350 km, 300 km detection range for an aircraft with an RCS of 16m² with track range of 150 km for an aircraft with an RCS 5m² with a LDSD detection range of 50-70 km for 16m² and a LDSD track range of 40-60 km for an aircraft with an RCS of 3m² with a rangefinding radar gun engagement range up to 10 km with max ground detection up to 200 km and track range for tank sized targets up to 25 km with tracking of up to 2 ground targets with a tracking scan range of 80° in azimuth and ±25° in elevation with a full tracking scan sweep in 3 seconds with ground mapping up to 200 km, with base image resolutions of 3, 30 and 300 m at a spatial resolution size of 50, 100 and 150 km with radar imaging complete in 30 seconds with max tracking target velocity at over 2500 kph and stores tracking information for up to 4 non tracked targets with predictive flight paths for non tracked targets up to 10 seconds with LDSD ground clutter rejection of 70> dB and low chaff rejection with a MTBF of 100 to 200 hours. OLS-30 fully stabilised sight with a fully digital electro optical system with a 4× optical magnification with an FOV of 18.75° and a 10× optical magnification with an FOV of 7.5° with an independent stabilised vertical movement of -15°/+30° and independent stabilised horizontal movement of 120° with a moving stabilisation accuracy of ±0.1 mils in azimuth and elevation and minimum /maximum stabilised sight movements of 0.03/60 deg/s with an angular tracking rate of 10 to 20 deg/s with FLIR enabling a max range of 20 km, detection of tank sized targets up to 10 km and identification up to 2 km with detection of corvette sized warships up to 16 km with identification up to 10 km with detection of fighter sized targets up to 13 km and identification up to 2 km, TV sight enabling a max range of 15 km with detection of tank sized targets up to 8 km and identification up to 6 km with detection of fighter sized targets up to 10 km and identification up to 8 km with NFOV detection of corvette sized warships up to 13 km with identification up to 11 km, IRST with tracking of up to 2 targets and automatic target tracking with an angular resolution of 0.1° and max tracking rate of 120 deg/s enabling a max detection range up to 120 km with a 70 to 100 km detection range and 20 to 40 km rear track range with 15 km front track range for fighter sized targets and a 20 km track range for ground targets and laser targeting with laser rangefinding, laser designation and laser spot tracking with an accuracy of 5m with a 15 km engagement range for aircraft and 20 km engagement range for ground targets. NSTs-T-04 HMD with a 160° horizontal FOV and ±40° vertical FOV up to 10 km)


Counter Measures: L-006M/SPO-15LM Beryoza-LM 2nd Generation digital RHAWS with 8 targets tracked with 6 preprogrammed threat identifiers and 5× receivers enabling a self protection envelope of 360° in azimuth and ±60° in elevation with band coverage of 4.4-10.3 GHz with a signal detectability range up to 225 km. SSP-2I digital fire countermeasure system. K-36DM Zero-Zero ejection seat. APP-50 countermeasure dispenser utilising 1st Generation IRCM and RFCM with 192 total rounds using the PPR-50 composite aluminium chaff that activates in 0.3 seconds and creates a false target RCS of greater than 60m² and using the PPI-50 thermite based flare with a minimum burn time of 3 seconds. SO-69/SRZO-2P 2nd Generation solid state IFF interrogator / transponder linked to the Parol fully digital IFF system with aircraft ID, full digital data encryption, reprogramming and cryptographic encoding. P-591 digital ICAS. KKO-15LP digital full ECLSS. 


(SM, KUB and 33M model adds L-150/SPO-32 Pastel 3rd Generation fully digital RHAWS with 16 targets tracked and 128> preprogrammed threat identifiers with guidance of up to 6 ARMs with 2 fired simultaneous and 10× receivers enabling a self protection envelope of 360° in azimuth and ±60° in elevation with band coverage of 1.2-18 GHz with a signal detectability range up to 320 km. SO-72/SRZO-2P 2nd Generation digital IFF interrogator/transponder linked to the Parol-2D fully digital IFF system with aircraft ID, full digital data encryption, radio/inertial navigation locating, reprogramming and cryptographic encoding. APP-50M countermeasure dispenser utilising 2nd Generation IRCM and RFCM with 192 total rounds using the PPR-50-17 composite aluminium jammer assisted chaff that activates in 0.3 seconds and creates a false target RCS of greater than 60m² and using the PPI-50-3 spectral flare with a minimum burn time of 3 seconds)


(SM3 model adds L-150NU-27/SPO-32M Pastel-M 4th Generation fully digital data fused RHAWS with 20 targets tracked with 242> preprogrammed threat identifiers with guidance of up to 8 ARMs with 4 fired simultaneous with 16× receivers enabling a self protection envelope of 360° in azimuth and ±180° in elevation with band coverage of 0.2-20 GHz with a signal detectability range up to 440 km)


(From early 2020s onwards Parol-2D is replaced by Password-3 all digital IFF system with low observability data sharing, satellite navigation locating, full digital data encryption, reprogramming and cryptographic encoding)


Electronic Warfare: L-005S Sorbitsya-S 3rd Generation digital SPJ with monopulse countermeasure, continuous wave countermeasure and pulse doppler countermeasure ECCM with track breaker, track breaking and blip enhancement ELINT with 4× receivers enabling an ECCM protection envelope of 360° in azimuth with a self protection jamming range of 200 km> with SPS-171 3rd Generation digital active jamming system operating on 6-10 GHz with deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, cross eye jamming and spot jamming jamming ECM with 4× PESA pyramidal horn antenna ECM transmitters enabling an active jamming range of 200 km>. 



(SM3 model adds L-175U Khibiny-U 4th Generation fully digital SPJ utilising radio direction finder with AoA and PRF determination, simultaneous monopulse countermeasure, continuous wave countermeasure, pulse doppler countermeasure and LPIR countermeasure with doppler shifting, home on jam and anti burn though ECCM with track breaker, advanced decoy generation, blip enhancement and global navigation spoofing ELINT with 8× receivers enabling a passive ECCM protection envelope of 360° in azimuth with a self protection jamming range of 300 km> with SAP-518 4th Generation fully digital active jamming system operating on 5-18 GHz with frequency agile deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, cross eye jamming, spot jamming, wave jamming, power managed jamming and DRFM jamming ECM with 4× GaAs AESA pyramidal horn ECM transmitters enabling an active jamming range of 300 km>) 


Guns: GSh-30-1 30mm autocannon slaved to laser rangefinder and radar with an effective firing range up to 2 km.


Ordinance Capacity: 10× hardpoints with a max 4400 kg munition capacity and 150 rounds for the gun. 


(SM3 model adds 12× hardpoints with a max 7000 kg munition capacity and 150 rounds for the gun)


Common Air to Air Payloads 

● 8× APU-470 racks with R-27R 2× APU-73 racks with R-73

● 8× APU-470 racks with 6x R-27R and 2x R-27T 2× SPS-171  

● 6× APU-470 racks with R-27R 2× APU-73 racks with R-73 2× SPS-171  



R-27R

3rd Generation Radar Missile 

9B-1101 Inverse Monopulse X band Semi Active Seeker with a digital phase comparison antenna array with an INS utilising a radio correction data link with back up inertial operting guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a radio proximity fuse and back up impact detonation with a continuous rod warhead enabling a blast radius of 10-15 m²

~90 km max Range at 10 km+ altitude 

~70 km max Range at 5 km+ altitude 

~50 km max Range at sea level 

~30 km engagement range vs RCS of 5m² at sea level 

~50 km engagement range vs RCS of 5m² at 5 km+ altitude 

~70 km engagement range vs RCS of 5m² at 10 km+ altitude 

~10 km NEZ range vs RCS of 5m² at sea level 

~20 km NEZ range vs RCS of 5m² at 5 km> altitude

~30 km NEZ range vs RCS of 5m² at 10 km> altitude

~Mach 4 at 5 km+ altitude 

~Mach 2 at sea level 

~Targeting Angles 35°

~Turn Rate 20 to 50 Deg/s

~Initial Acceleration of 210-370 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 74g 


R-27T 

4th Generation IR Missile 

Geofizika-36T LN² Cooled digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~70 km max Range at altitude 

~40 km max Range at sea level 

~60 km engagement range 

~All aspect lock range 5 km

~Rear aspect lock range 20 km

~Mach 4 at high altitude 

~Mach 2 at sea level 

~Rectile Speed: 125 Hz

~Flare rejection 0.6

~Gimbal limit: 55°

~Angular Tracking: 60 deg/s 

~Turn Rate 20 to 50 Deg/s

~Initial Acceleration of 210-370 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 74g 


R-73

4th Generation IR Missile 

Mayak-80 LN² Cooled digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~30 km max Range at 5 km> altitude 

~20 km max Range at sea level 

~20 km engagement range at 5 km>

~All aspect lock range 4 km

~Rear aspect lock range 10 km 

~Rectile Speed: 150 Hz

~Mach 3 at high altitude 

~Mach 2 at sea level 

~Flare rejection 0.6

~Gimbal limit: 45°

~Angular Tracking: 60 deg/s 

~Turn Rate 90 to 120 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 60g 


GSh-30-1

9A-4071K 30×165mm SAPHEI


K, 33 and 90+ model adds 

● 6× AKU-170 racks with R-77 2× APU-73 racks with R-74 2× SAP-518 

● 4× APU-470 racks with R-27ER 4× AKU-170 racks with R-77 2× APU-73 racks with R-74


R-77

4th Generation Radar Missile 

9P-1348 Inverse Monopulse X band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a radio correction data link with back up inertial operting guidance, home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a Z23nA radio proximity fuse and back up impact detonation with with a high explosive blast warhead enabling a blast radius of 10-15 m²

~150 km max Range at 10 km+ altitude 

~120 km max Range at 5 km+ altitude 

~58 km max Range at sea level 

~35 km engagement range vs RCS of 5m² at sea level 

~80 km engagement range vs RCS of 5m² at 5 km+ altitude 

~110 km engagement range vs RCS of 5m² at 10 km+ altitude 

~15 km NEZ range vs RCS of 5m² at sea level 

~25 km NEZ range vs RCS of 5m² at 5 km> altitude

~30 km NEZ range vs RCS of 5m² at 10 km> altitude

~6 km ARH lock range vs RCS of 1m²

~18 km ARH lock range vs RCS of 5m²

~24 km ARH lock range vs RCS of 10m²

~0.1 m² minimum target RCS for ARH lock 

~Mach 4 at high altitude 

~Mach 2 at sea level 

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~50g Overload Tolerance 

~8g launch limiter

~12g target limiter 


R-27ER

3rd Generation Radar Missile 

9B-1101E Inverse Monopulse X band Semi Active Seeker with a fully digital phase comparison antenna array with an INS utilising a radio correction data link with back up inertial operting guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a radio proximity fuse and back up impact detonation with a continuous rod warhead enabling a blast radius of 10-15 m²

~130 km max Range at 10 km+ altitude 

~110 km max Range at 5 km+ altitude 

~90 km max Range at sea level 

~70 km engagement range vs RCS of 5m² at sea level 

~90 km engagement range vs RCS of 5m² at 5 km+ altitude 

~110 km engagement range vs RCS of 5m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 5m² at sea level 

~30 km NEZ range vs RCS of 5m² at 5 km> altitude

~50 km NEZ range vs RCS of 5m² at 10 km> altitude

~Mach 5 at high altitude 

~Mach 2 at sea level 

~Targeting Angles 35°

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~60g Overload Tolerance 

~8g launch limiter 

~10g target limiter 


R-27ET 

4th Generation IR Missile 

Geofizika-36TE LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~120 km max Range at altitude 

~40 km max Range at sea level 

~80 km engagement range 

~All aspect lock range 20 km

~Rear aspect lock range 30 km

~Mach 5 at high altitude 

~Mach 2 at sea level 

~Rectile Speed: 125 Hz

~Flare rejection 0.6

~Gimbal limit: 55°

~Angular Tracking: 60 deg/s 

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 60g 


R-74

4th Generation IR Missile 

Mayak-80B LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~30 km max Range at 5 km> altitude 

~20 km max Range at sea level 

~20 km engagement range at 5 km> 

~All aspect lock range 6 km

~Rear aspect lock range 10 km

~Mach 3 at high altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.6

~TVC: Yes turns 180° / 3 seconds 

~Gimbal limit: 60°

~Angular Tracking: 60 deg/s 

~Turn Rate 90 to 120 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 60g 



SM and KUB model adds 

● 6× AKU-170 racks with R-77-1 2× APU-73 racks with R-74M 2× SPS-171


R-77-1A

4th Generation Radar Missile 

9B-1248 Inverse Monopulse X band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a bi-directional radio correction data link with back up inertial operting guidance, home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser and Z23nA radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~150 km max Range at 10 km+ altitude 

~120 km max Range at 5 km+ altitude 

~90 km max Range at sea level 

~50 km engagement range vs RCS of 5m² at sea level 

~90 km engagement range vs RCS of 5m² at 5 km+ altitude 

~120 km engagement range vs RCS of 5m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 5m² at sea level 

~30 km NEZ range vs RCS of 5m² at 5 km> altitude

~40 km NEZ range vs RCS of 5m² at 10 km> altitude

~6 km ARH lock range vs RCS of 1m²

~18 km ARH lock range vs RCS of 5m²

~24 km ARH lock range vs RCS of 10m²

~0.1 m² minimum target RCS for ARH lock 

~Mach 4 max target velocity

~Mach 4 at high altitude 

~Mach 2 at sea level 

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~Launch limiter 9g 

~Target limiter 12g 

~Overload Tolerance 60g


R-74M

4+ Generation IR Missile 

Impuls-90 LN² Cooled NIR & UV channel fully digital pseudo-imaging HgCdTe Seeker with dual band, gatewidth and seeker shut off IRCCM

~50 km max Range at 5 km> altitude 

~40 km max Range at sea level 

~40 km engagement range at 5 km> altitude

~All aspect lock range 10 km

~Rear aspect lock range 10 km 

~Mach 3 at 5 km> altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.8

~Gimbal limit: 75°

~Angular Tracking: 60 deg/s 

~Turn Rate 120 to 180 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 80g 



SM3 adds 

● 8× AKU-170 racks with R-77-1 2× APU-73 racks with R-74M 2× SAP-518


R-77-1B

4+ Generation Radar Missile 

9B-1103M-150 Inverse Monopulse X/Ku band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a bi-directional radio correction data link with back up inertial operting guidance, dual band, home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser and Z23nA radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~200 km max Range at 10 km+ altitude 

~150 km max Range at 5 km+ altitude 

~80 km max Range at sea level 

~50 km engagement range vs RCS of 5m² at sea level 

~110 km engagement range vs RCS of 5m² at 5 km+ altitude 

~140 km engagement range vs RCS of 5m² at 10 km+ altitude 

~30 km NEZ range vs RCS of 5m² at sea level 

~40 km NEZ range vs RCS of 5m² at 5 km> altitude

~60 km NEZ range vs RCS of 5m² at 10 km> altitude

~8 km ARH lock range vs RCS of 1m²

~20 km ARH lock range vs RCS of 5m²

~26 km ARH lock range vs RCS of 10m²

~0.05 m² minimum target RCS for ARH lock 

~Mach 5 max target velocity 

~Mach 4 at high altitude 

~Mach 2 at sea level 

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~Launch limiter 9g 

~Target limiter 12g 

~Overload Tolerance 60g



R-27ET 

4th Generation IR Missile 

Geofizika-36TE LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~120 km max Range at altitude 

~40 km max Range at sea level 

~80 km engagement range 

~All aspect lock range 20 km

~Rear aspect lock range 30 km

~Angular tracking 60 deg/s

~Mach 4 at 10 km+ altitude 

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Rectile Speed: 125 Hz

~Flare rejection 0.6

~Gimbal limit: 55°

~Angular Tracking: 60 deg/s 

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~Launch limiter 7g 

~Target limiter 8g 

~Overload Tolerance 70g 


R-74M

4+ Generation IR Missile 

Impuls-90 LN² Cooled NIR & UV channel fully digital pseudo-imaging HgCdTe Seeker with dual band, gatewidth and seeker shut off IRCCM

~50 km max Range at 5 km> altitude 

~40 km max Range at sea level 

~40 km engagement range at 5 km> altitude

~All aspect lock range 10 km

~Rear aspect lock range 10 km 

~Mach 3 at 5 km> altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.8

~Gimbal limit: 75°

~Angular Tracking: 60 deg/s 

~Turn Rate 120 to 180 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 80g 

Laser Guided Bombs 

KAB-500L 1st Generation LG HE  

KAB-500L-Pr-E 2nd Gen Bunker Buster 

KAB-500L-F-E 1st Generation FRAG-HE 

KAB-500L-OD-E 1st Generation FAE 

KAB-500L-K-E 1st Generation Cluster Bomb 


Optically Guided Bombs 

KAB-500Kr 2nd Generation HE

KAB-500Kr-Pr-E 2nd Gen Bunker Buster 

KAB-500Kr-F-E 2nd Generation FRAG-HE 

KAB-500Kr-OD-E 2nd Generation FAE 

KAB-500Kr-K-E 2nd Generation Cluster Bomb


Air to Ground Missiles 

Kh-59-M 3rd Generation HE Cruise Missile

Kh-59-K 3rd Generation HEAT Cruise Missile

Kh-59-KE 3rd Gen Cluster Cruise Missile

Kh-59L-M 2nd Gen Laser Guided HE

Kh-59L-K 2nd Gen Laser Guided HEAT

Kh-59L-KE 2nd Gen Laser Guided Cluster 

Kh-59T-M 2nd Generation OG HE

Kh-59T-K 2nd Generation OG HEAT

Kh-59T-KE 2nd Generation OG Cluster 

Kh-29T-M 2nd Generation OG HE

Kh-29T-K 2nd Generation OG HEAT 

Kh-29L-M 2nd Generation Laser Guided HE 

Kh-29L-K 2nd Generation Laser Guided HEAT 


Unguided Bombs 

FAB-500 HE bomb

FAB-250  HE bomb

BETAB-500 bunker buster

RBK-500 cluster munition bomb

RBK-250 cluster munition bomb

KMGU cluster munition dispenser 


Rockets 

S-13 KEP Rocket 

S-13T HEAT Rocket 

S-24 HE-FRAG 


Later models add 


R-77-1C

4+ Generation Radar Missile 

9B-1103M-200PA Inverse Monopulse Ku band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a bi-directional radio correction data link with back up inertial operting guidance, home on jam, multimode guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser and Z23nA radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~200 km max Range at 10 km+ altitude 

~150 km max Range at 5 km+ altitude 

~80 km max Range at sea level 

~50 km engagement range vs RCS of 3m² at sea level 

~100 km engagement range vs RCS of 3m² at 5 km+ altitude 

~120 km engagement range vs RCS of 3m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 3m² at sea level 

~40 km NEZ range vs RCS of 3m² at 5 km> altitude

~60 km NEZ range vs RCS of 3m² at 10 km> altitude

~10 km ARH lock range vs RCS of 1m²

~20 km ARH lock range vs RCS of 3m²

~30 km ARH lock range vs RCS of 10m²

~0.05 m² minimum target RCS for ARH lock 

~Mach 5 max target velocity 

~Mach 4 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~Launch limiter 9g 

~Target limiter 12g 

~Overload Tolerance 60g



Su-27 (Prototype) 

Su-27S (Production)

Su-27SM 
Su-27SM3
Su-27K

Su-27KUB

Su-27UB 

Su-33 




MiG-35 Super Fulcrum Series 


MiG-35

Prototype: 2007

Completed: 2019

Production: 2021

Generation: 4.5

Aircraft Role: MultiRole/Strike Fighter 

Number Made: 10

Combat Rank: D


Engines and Airframe: CAD composite construction LV Airframe with an RCS minimum of 1m². Crew of 1-2. Length 17.3 m. Height 4.4 m. Wingspan 12 m. Wing area 45 m². Frame weight 12,000 kg. Takeoff weight 24,500 kg. Max Fuel 4,500 kg 2× Klimov RD-33MKB axial flow high bypass FADEC turbofans with 112 kN of thrust and 180 kN of thrust in afterburner. Service Ceiling up to 18 km. 


Speed and Endurance: Top speed of mach 2.1 to 2.4 at 15 km+, mach 2 to 2.3 at 10 km+, mach 1.9 to 2 to at 5 km+ and mach 1 to 1.2 at sea level. Service Ceiling of 17 to 23 km. Combat range of 900-1100 km. Refueling boom. Acceleration 6-13 seconds to mach 1 at sea level. Stall speed 90-130 kph. Take off distance is 300m with ATA payload to 700m for full payload. Landing distance 500 to 700m. In flight refueling. 


Stealth: low visibility airframe, leading edge trails and full RAM applied to engines front and sides. 


Airframe RCS 

RCS Minimum: 1m²

RCS Median: 1.5m²

RCS Average: 2-5m²


Manuvarabilities: Thrust to weight ratio of 1.1 at full air to air payload and 1.4 at half fuel/loadout and 0.9 at full loadout. Roll rate of 140 deg/s at high speed and 250 deg/s at low speed. Climb rate of 260-310 m/s. Angle of Attack at 30° at mach 2>, 50° at mach 1> and 70° at mach <1. 10 to 40 kph/s speed bleed at high g instantaneous maneuvers and 5 to 15 kph/s speed bleed at high g sustained maneuvers. Wing loading of 370-390 kg/m². Sustained G tolerance of 9g and an Overload Tolerance of 13g and wing break at 19.5-26g. 4× LERXs with pitch of ±60°.and 2× elevators with pitch of -60°.


(Can be fitted with KliVT 3D thrust vectoring system with ±18° in roll/yaw and pitch with deflection at 30 deg/s)


Aircraft Turn Rates 


Sustained turn rates 


Mach ~1.5 Speeds 

● 2-3 deg/s at 10 km altitude 

● 4-6 deg/s at 5 km altitude 

● 7-10 deg/s at sea level   


Mach ~1 Speeds 

● 13-14 deg/s at 10 km altitude 

● 16-18 deg/s at 5 km altitude 

● 17-20 deg/s at sea level   


Mach ~0.5 Speeds 

● 13-15 deg/s at 10 km altitude 

● 16-19 deg/s at 5 km altitude 

● 20-24 deg/s at sea level   


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 4-5 deg/s at 10 km altitude 

● 6-8 deg/s at 5 km altitude 

● 9-12 deg/s at sea level  


Mach ~1 Speeds 

● 15-17 deg/s at 10 km altitude 

● 18-21 deg/s at 5 km altitude 

● 20-24 deg/s at sea level  


Mach ~0.5 Speeds 

● 23-25 deg/s at 10 km altitude 

● 26-30 deg/s at 5 km altitude 

● 30-35 deg/s at sea level  



With KliVT fitted 


Aircraft Turn Rates 


Sustained turn rates 


Mach ~1.5 Speeds 

● 4-7 deg/s at 10 km altitude 

● 6-10 deg/s at 5 km altitude 

● 12-15 deg/s at sea level   


Mach ~1 Speeds 

● 16-18 deg/s at 10 km altitude 

● 19-21 deg/s at 5 km altitude 

● 22-25 deg/s at sea level   


Mach ~0.5 Speeds 

● 18-20 deg/s at 10 km altitude 

● 21-24 deg/s at 5 km altitude 

● 25-29 deg/s at sea level   


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 14-15 deg/s at 10 km altitude 

● 16-18 deg/s at 5 km altitude 

● 19-22 deg/s at sea level  


Mach ~1 Speeds 

● 25-27 deg/s at 10 km altitude 

● 28-31 deg/s at 5 km altitude 

● 30-34 deg/s at sea level  


Mach ~0.5 Speeds 

● 33-35 deg/s at 10 km altitude 

● 36-40 deg/s at 5 km altitude 

● 40-45 deg/s at sea level  


Navigation & Flight Control: PNS-29M fully computerised nav/attack suite with a SAU-458 6× axis computerised autopilot and a KSU-941M fully digital fly by wire AFCS utilising a 64x bit digital ADC with an IVS-29-2 digital navigation system utilising a BINS-SP2M 64x bit fully digital navigation computer using a fully digital INS utilising a ring laser gyroscope, hemispherical resonator gyroscope and fiber optic gyroscope with an accuracy of 0.005° in pitch, yaw and heading with an error rate of 0.01 km/ph and velocity error rate of <0.1 m/s with a hybridised position accuracy of <1m RSBN-85VM Vstrecha-M fully digital radio navigation system with DVOR and ILS with a position accuracy of <10m and angular accuracy of ±0.01°. MFI-25Sh 5th Generation cockpit with 1× UHD LCD MFD and HOTAS control stick. ZSh-7AP Flight Helmet. ARK-35 fully digital ADF. RV-22 fully digital radar altimeter. PPA-S/V-KNS GLONASS-K Global navigation satellite system with a max CEP of 60cm and average CEP of 3m. (When inside former USSR airspace SDCM GNSS augmentation improves precision with a max accuracy of 10cm and average accuracy of <1m) Zhuk fully digital navigation radar. 


(UB trainer model has MFI-25 5th Generation cockpit 6× UHD LCD MFDs and HOTAS control stick)


Fire Control: SUO-35 fully computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with fully digital sensors with full stability augmentation with the KPrNO-35 sensor fusion system utilising NAV, RDR, IRST, EOT, TDL, IFF, RHAWS, RFCM, IRCM, MAW, ESM and ECM information displayed on one screen with radar targeting fusion utilising RLPK-29M2 radar targeting and OLS-UEM electro optical, laser and infrared imaging/tracking targeting with a SOLO-35 all digital FCC with KOMDIV-64 64x bit 2× core CPUs performing 10-20b IPS and 150-200b FLOPS. TsVB-54 all digital ballistic computer utilising a KOMDIV-64 64x bit 2× core CPU enabling fully digitised automatic digital target lead and gun and missile coursing with gun, rocket and bomb CCRP and CCIP with a bomb and rocket accuracy of <3-5m CEP at a range up to 2000m and altitudes up to 5000m and <30-40m CEP at a range up to 10,000m and altitude up to 12,000m. FGA-29 Zhuk-A 5th Generation Radar utilising an electronically steered fully digital X band AESA system with a patch antenna array using a sensor fused system with programmable fully digital signal processing, digital beam forming, coherent doppler filtering and signal modulation based LDSD with and pulse doppler IFF, tactical & missile data link and SATCOM integration with CW illumination for SARH guidance, very low false alarm rates, BIST system and fully computerised radar image displaying with simultaneous multi-mode operation, simultaneous searching tracking and guidance, radar map freezing, raid assessment, active jamming, predictive flight path, non tracked target tracking, adaptive processing, automatic target recognition, air and ground based JEM, RCS and HRRP non cooperative target recognition functions and agile beam, raster, palmer, conical, sector, circular and spiral scan scanning modes utilising DBS, I/SAR, RBGM, GTD, MGMTT, TAR, TFR, STI and MGMTI air to ground radar modes, FTT, I/SAR, SSD and SSTT air to sea modes and SRC/LDSD, MR, LPIR, ATC, STTR, MTTR and HMD, LDR, IRST, EOT and multi target RFR based ACMs air to air radar modes with gain modulation, notch filtering, sidelobe suppression, polarization filtering, tunable frequency filters, frequency hopping, home on jam, jammer identification and phase coded pulse compression ECCM with 1016 GaAs T/R modules and a 688mm antenna diameter with an average power output of 3 kW and max power output of 8 kW and 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance, 1 channel for ECM with a noise factor of 3 dB. IKSh-1M 5th Generation HUD with a fully digital LCD glass display utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with an integrated digital bombing complex utilising gun, bomb and rocket CCRP and CCIP with gun EEGS and a digital MFD with electro optical slaving, mission control, navigation systems and weapons functions. 5th Generation Radar display with an SVD system utilising a high resolution full colour raster image displayed on a LCD MFD with computerised target generation, ECM resolution, navigation data and aircraft flight information with data link integration. ZSh-7AP Flight Helmet with NSTsI-KOS 2nd Generation HMD utilising automatic cueing for targeting with navigation and targeting data displayed with head tracking software. OLS-13SM-1 multi-channel fully digital EOTS with a FHD resolution TV sight with a ~1080p day time image resolution, 1.06 μm Nd:YAG auto adjusting laser targeting system with laser rangefinding, laser designation and laser spot tracking and a 3rd Generation IRST & 3rd Generation FLIR system utilising a LN² cooled infrared imaging QWIP detector with an FPA format of 320x240 and a thermal image resolution of 640×480p


(UB trainer models use RP-35 4th Generation Radar with a digital electronically steered X band PESA system with a patch antenna array with 658 total R/E modules with HPRF power output on average being 2-3 kW with a 8 kW max output with an 800 mm antenna diameter)


Communication & C2: S-107-1 fully digital unified communication complex with an R-999 fully digital software defined VHF/UHF and HF radio with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding, rekeying encryption, amplitude and phase shift keying, pulse code modulation and full digital data encryption with text, video, image and voice formats utilised operating on 99 programmable channels and 512 frequency carriers with data transfer speeds of 16 kbit/s, 10 mbit/s and 30 mbit/s utilising an integrated PPCh-B FHSS and CRNG system utilising up to 20,000 frequency hops per second and 12 round cryptographic encryption for 128 bit, 14 round cryptographic encryption for 192 bit and 16 round cryptographic encryption for 256 bit with an operating LOS communication range of 450 km and BLOS unlimited with satellite link and the OSNOD fully digital tactical data link linked to the NDMC NTsUO military command center utilising the YeESU-TZ military C4 network that organises coordination between the Kavkaz-EASS military C3I radio communication network, Voiska PVO-PRO air defence network, ASUNO-S artillery network, PTK and Svod blue force tracking networks, Glaz-Groza UAV network and the Bylina electronic warfare network with links to BARS, Orbita, Andromeda-D, Strelets-M, Sagittarius-M, Akatsiya-E, Akatsiya-M, Barnaul-T, Baikal-1ME, Universal-1E, Fundament-M and Polyana-D4M1 C2 softwares and VIP-117M3, Lvin, 4RT-S, Legend, Planet, Type-1B, Kulon-V and Baget-K data terminals with two way communication, low observability data exchange, weapons management, radio communication integration, navigation data, IFF integration, SATCOM integration, fullly digital data encryption, ECM resistance, multi aircraft link, multi platform subscription, frequency hopping, electronic countermeasure support and C4 integration utilising ground, air and sea based computer, radar and electro optically generated data exchange with high resolution text, image, and pre recorded sound formats used with live video and voice formats displayed on tactical display, with data transfer speeds of 1024 bit/s, 2048 bit/s, 40 kbit/s, 100 kbit/s and 34.4 mbit/s every 0.5 to 1 seconds operating on 300 MHz to 3 GHz with up to 80,000 frequency hops per second on 60 frequency carriers enabling a LOS data transmission range up to 500 km and BLOS up to 1500 km and unlimited range with satellite link with data exchange between up to 1800 subscribers and unlimited with satellite link. Baget-53-31M fully digital FMC utilising 1888TX018 64x bit 8× core CPUs performing 20-30b IPS and 300-400b FLOPS using the BagrOS-4000 4-5m SLOC RTOS using an IUS-35 C2ISR suite linked to the Voiska PVO-PRO air defence network and the YeESU-TZ military C4 network with section to platoon level blue force tracking software, C4 integration, SATCOM integration, GNSS integration, electronic countermeasure support, surrounding land formation intelligence, digital navigation, moving map display, precision targeting, integrated aircraft health management software, reconnaissance software, data sharing and C2 software. 


(2024 models onwards use Baget-53-31M1 fully digital FMC utilising Elbrus-16S 64x bit 16× core CPUs performing 30-40b IPS and 400-600b FLOPS for FMC) 


Targeting: Zhuk-A radar with a 120° horizontal and ±60° vertical scan range with tracking of 30 targets and data linking of 8 missiles enabling a 370 km Rmax range, in 15-24° STTR narrow beam mode detection range is 250 to 300 km vs RCS of 3m², 100 to 150 km vs RCS of 1m² and 60 to 80 km vs RCS of 0.1m², normal detection range of 260 km for an aircraft with an RCS of 5m² and 160 km track range for an aircraft with an RCS of 3m² with a LDSD detection range of 120 km for 3m² and a LDSD track range of 120 km for an aircraft with an RCS of 3m² with a rangefinding radar gun engagement range up to 20 km with a max ground detection range of 300 km and 90 km track range for tank sized targets with tracking of up to 4 targets with ground mapping up to 80 km, with base image resolutions of 0.5, 1 and 3 m at a spatial resolution size of 20, 60 and 80 km with radar imaging complete in 20 seconds with a tracking scan range of 120° in azimuth and ±60° in elevation with a full tracking scan sweep in 0.1 seconds with max tracking target velocity at over 7408 kph with LPI target acquisition with over 500 frequency hops per second and a max LPI engagement range of 160 km vs RCS of 3m² and stores tracking information for up to 15 non tracked targets with predictive flight paths for non tracked targets up to 14 seconds with LDSD ground clutter rejection of 120> dB, NCTR for 4 targets up to 60> km with a scan range of ±30° in azimuth and ±15° in elevation with up to 200 preprogrammed target identifiers and very high chaff rejection with a MTBF of 500 to 900 hours. OLS-13SM-1 fully stabilised sight with a fully digital electro optical system with a 4× optical magnification with an FOV of 18.75° and a 10× optical magnification with an FOV of 7.5° with an independent stabilised vertical movement of -15°/+60° and independent stabilised horizontal movement of 180° with a moving stabilisation accuracy of 0.05 mils in azimuth and elevation and minimum/maximum stabilised sight movements of 0.03/60 deg/s with an angular tracking rate of 60 deg/s with FLIR enabling a max range of 30 km, detection of tank sized targets up to 12 km and identification up to 3 km with detection of corvette sized warships up to 28 km with identification up to 20 km with detection of fighter sized targets up to 20 km and identification up to 4 km with an automatic target tracking range up to 8 km, TV sight enabling a max range of 20 km, detection of tank sized targets up to 13 km and identification up to 10 km with detection of fighter sized targets up to 16 km and identification up to 14 km with NFOV detection of corvette sized warships up to 18 km with identification up to 15 km with identification up to 25 km, IRST with automatic target tracking, automatic target slaving and automatic target recognition with tracking of 2 targets with an Angular resolution of 0.05° and max tracking rate of 200 deg/s enabling a max range up to 150 km with a 80 to 120 km detection range and 40 to 60 km rear track range with 15 km front track range for fighter sized targets and a 30 km track range for ground targets and laser targeting system with laser rangefinding, laser designation and laser spot tracking with an accuracy of ±5m with with a 15 km engagement range for aircraft and 20 km engagement range for ground targets.  NSTsI-KOS HMD with a 170° horizontal FOV and -35°/+85° vertical FOV with a target engagement range up to 20 km. 


(UB trainer models have RP-35 radar with a 140° horizontal and ±70° vertical scan range enabling an Rmax range up to 300 km, 200 km detection range for 5m² with a 120 km track range for an aircraft with an RCS of 3m² with tracking of up to 24 targets and data linking of 6 missiles with a max ground detection range of 160 km and 60 km track range for tank sized targets with tracking of up to 16 targets and locking and firing of up to 4 with an tracking scan range up to 80° with a full horizontal scan sweep in over 0.2 seconds with max tracking target velocity at over 7408 kph with LDSD ground clutter rejection of 70> dB.)


Targeting Pods 


NPK-SPP OLS-K 3rd Generation Targeting Pod with Raguga-V 3rd Generation infrared imaging with a 1PN136 matrix utilising a 384x388 FPA format with a thermal image resolution of 768×776p with fully automated target tracking and an integrated Nd:YAG 3rd Generation LDR and FHD EOTS with EOTS with tracking of up to 30 targets and locking of up to 8 with FLIR enabling a max range of 30 km, detection of tank sized targets up to 12 km and identification up to 3 km with detection of corvette sized warships up to 28 km with identification up to 20 km with detection of fighter sized targets up to 20 km and identification up to 4 km LDR with a 40 km engagement range for ground targets. 



T-220I 3rd Generation Targeting Pod with FHD EOTS with a ~1440p day time image resolution, Raduga-V 3rd Generation FLIR system utilising a 1PN136 matrix with a 388x384 FPA format, 776×768p thermal image resolution, 3-5 μm spectral range, pixel pitch of 15 μm, NETp of 30 mK and 50 Hz refresh rate with an integrated auto adjusting Nd:YAG laser targeting system with laser rangefinding, laser designation and laser spot tracking with an accuracy of 10m with utilising a fully digital telescopic electro optical sight with a day time 4× optical magnification with an FOV of 25°, 60× optical magnification with an FOV of 1.6° and a 120× electro optical magnification with an FOV of 0.8° with a night time 1× optical magnification with an FOV of 24°, 10× optical magnification with an FOV of 2.4° and a 20× optical magnification with an FOV of 1.2° with independent stabilised depth movement, an independent stabilised vertical movement of -170°/+10° and independent stabilised horizontal movement of 320° with a moving stabilisation accuracy of 0.05 in elevation and azimuth and minimum/ maximum stabilised sight movements of 0.01/60 deg/s with an angular tracking rate of 50 to 90 deg/s with tracking of up to 30 targets and locking of up to 8 with FLIR enabling a max range of 30 km, detection of tank sized targets up to 12 km and identification up to 3 km with detection of corvette sized warships up to 28 km with identification up to 20 km with detection of fighter sized targets up to 20 km and identification up to 4 km with automatic target tracking up to 8km , TV sight enabling a max range of 90 km, detection of tank sized targets up to 50 km and identification up to 45 km with detection of fighter sized targets up to 70 km and identification up to 60 km with detection of corvette sized warships up to 87 km with identification up to 80 km with a 40 km laser engagement range for ground targets. 


Countermeasures: L-150NU-35/SPO-32M Pastel-M 4th Generation fully digital data fused RHAWS with 20 targets tracked with 242> preprogrammed threat identifiers with guidance of up to 8 ARMs with 4 fired simultaneous with 16× receivers enabling a self protection envelope of 360° in azimuth and ±180° in elevation with band coverage of 0.2-20 GHz with a signal detectability range up to 440 km. 6× SOAR IR MAW receivers covering a spectral range of 3 to 5 µm enabling a protection envelope of 360° in azimuth and ±180° in elevation with a launch detection range of 70 km> and course trajectory detection range of <9 km. 4× SOLO laser warning receivers covering a pulse repetition frequency of 0.1 to 70 Hz and pulse duration of 60 ks and spectral range of 0.9 to 1.7 µm enabling a protection envelope of 360° in azimuth and ±90° in elevation. BVP-30-26M countermeasure dispenser utilising 2nd Generation IRCM and RFCM with 60 total rounds using the PPR-26-51 composite aluminium jammer assisted chaff that activates in 0.3 seconds and creates a false target RCS of greater than 60m² and using the PPI-26-2-1 spectral flare with a minimum burn time of 3 seconds. Blesna Diamant-S 3rd Generation RFCM with a towed decoy SPJ with a 100m towing range utilising simultaneous LPIR, monopulse, continuous wave and pulse doppler countermeasure. K-36D-5 Zero-Zero ejection seats. SO-96/SRZ-035M 3rd Generation fully digital IFF interrogator/transponder linked to the Password-3 fully digital IFF system with aircraft ID, low observability data sharing, satellite navigation locating, full digital data encryption, reprogramming and cryptographic encoding SOZhE-35 all digital ICAS, full ECLSS and fire countermeasure system. 


Electronic Warfare: L-203 Gardenia-2 5th Generation fully digital ECM System with an SPJ suite utilising radio direction finder with AoA and PRF determination, simultaneous monopulse countermeasure, continuous wave countermeasure, pulse doppler countermeasure and LPIR countermeasure with doppler shifting, noise cloaking, home on jam, anti burn though and self jam resistance ECCM with 8× receivers enabling an ECCM protection envelope of 360° in azimuth with a self protection jamming range of 300 km> with an active jamming system operating on 2-20 GHz with frequency agile deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, spot jamming, wave jamming, power managed jamming and DRFM/ISRJ jamming ECM with track breaker, advanced decoy generation, blip enhancement, satellite interception and global navigation spoofing ELINT and a GaAs AESA patch antenna ECM transmitter with an active jamming range of 300 km>.  


Guns: GSh-30-1 30mm autocannon slaved to laser rangefinder and radar with an effective firing range up to 2 km. 


Ordinance Capacity: 9× hardpoints with a max 8000 kg munition capacity and 100 rounds for the gun. 


Common Air to Air Payloads 

● 7× AKU-170 racks with R-77M 2× APU-73 racks with R-74M2


R-77M

5th Generation Radar Missile 

9B-1103M2 Ka/Ku band AESA Active Seeker with 64 GaAs T/R modules using a fully digital patch antenna array with an INS/GNSS utilising a bi-directional radio correction data link with back up inertial operting guidance, LPIR, home on jam, dual band seeker and polarisation filtering ECCM utilising a solid fuel dual pulse rocket motor with a laser and radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~300 km max Range at 10 km+ 

~250 km max Range at 5 km+

~150 km max Range at sea level 

~120 km engagement range vs RCS of 1m² at sea level 

~190 km engagement range vs RCS of 1m² at 5 km+ altitude 

~220 km engagement range vs RCS of 1m² at 10 km+ altitude 

~50 km NEZ range vs RCS of 1m² at sea level 

~70 km NEZ range vs RCS of 1m² at 5 km> altitude

~90 km NEZ range vs RCS of 1m² at 10 km> altitude

~2 km ARH lock range vs RCS of 0.003m²

~14 km ARH lock range vs RCS of 1m²

~26 km ARH lock range vs RCS of 3m²

~35 km ARH lock range vs RCS of 10m²

~0.0005 m² minimum target RCS for ARH lock 

~Mach 6 max target velocity 

~Mach 5 top speed above 5 km altitude 

~Mach 3 top speed at sea level

~Targeting Angles 60°

~Turn Rate 70 to 120 Deg/s

~Initial Acceleration of 300-600 m/s>

~Launch limiter 10g 

~Target limiter 12g 

~Overload Tolerance 80g


R-74M2

5th Generation IR Missile 

Karfagen-760 LN² Cooled MIR & UV channel fully digital pseudo-imaging HgCdTe LOAL Seeker with dual band, MITL, IOG, gatewidth and seeker shut off IRCCM

~60 km max Range 

~50 km range at sea level 

~50 km engagement range 

~All aspect lock range 10 km

~Rear aspect lock range 10 km

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Flare rejection 0.9+

~Turn Rate 120 to 180 Deg/s

~Initial Acceleration of 300-400 m/s>

~Rectile Speed: 200 Hz

~Gimbal limit: 180°

~Angular Tracking: 75 deg/s 

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 80g


Air to Ground Missiles  

Kh-69 LO 4th Gen Cluster Cruise Missile 

Kh-69 LO 4th Gen HEAT Cruise Missile 

Kh-59MK2-F-E LO 3rd Gen OG/IIR FRAG-HE 

Kh-59M2-M 2nd Generation OG HE 

Kh-59M2-K 2nd Generation OG HEAT 

Kh-59M2-KE 2nd Generation OG Cluster 

Kh-59M2D-M 2nd Generation OG/IIR HE 

Kh-59M2D-K 2nd Generation OG/IIR HEAT 

Kh-59M2D-KE 2nd Generation OG/IIR Cluster 

Kh-59MK-M 4th Generation HE Cruise Missile

Kh-59MK-K 4th Gen HEAT Cruise Missile

Kh-59MK-KE 4th Gen Cluster Cruise Missile

Kh-58UShKE 3rd Gen Anti Radiation  

Kh-58UShKE-TP 3rd Gen OG/IIR Anti Radiation

Kh-29MP-M 4th Gen HE Ballistic Missile 

Kh-29MP-K 4th Gen HEAT Ballistic Missile 

Kh-29TE-M 3rd Generation OG HE 

Kh-29TE-K 3rd Generation OG HEAT 

Kh-29TD-M 3rd Generation OG/IIR HE 

Kh-29TD-K 3rd Generation OG/IIR HEAT 

Kh-29ML-M 3rd Generation Laser Guided HE 

Kh-29ML-K 3rd Gen Laser Guided HEAT   


Bunker Busters 

Kh-59MKM 3rd Generation Bunker Buster 

Kh-59MK2-Pr LO 3rd Gen Bunker Buster 

KAB-500Kr-Pr-E 2nd Gen Bunker Buster 

KAB-500LG-Pr-E 2nd Gen Bunker Buster

KAB-250LG-Pr-E 2nd Generation Bunker Buster

BETAB-500SHP 1st Generation bunker buster

BETAB-500 1st Generation Bunker buster 

BETAB-500Y 1st Generation Bunker buster 


Laser Guided Bombs 

KAB-20LG-K 3rd Generation HEAT 

KAB-20LG-FE 3rd Generation FRAG-HE  

KAB-50LG-K 3rd Generation HEAT 

KAB-50LG-FE 3rd Generation FRAG-HE  

KAB-100LG-K 3rd Generation HEAT 

KAB-100LG-FE 3rd Generation FRAG-HE 

KAB-250LG 3rd Generation HE 

KAB-250LG-F-E 3rd Generation FRAG-HE 

KAB-250LG-OD-E 3rd Generation FAE

KAB-500MLG 3rd Generation HE

KAB-500MLG-Pr-E 3rd Gen Bunker Buster 

KAB-500MLG-F-E 3rd Generation FRAG-HE 

KAB-500MLG-OD-E 3rd Generation FAE 

KAB-500MLG-K-E 3rd Gen Cluster Bomb


Optically Guided Bombs 

KAB-50Kr-M-K 3rd Generation HEAT 

KAB-50Kr-MT-K 3rd Generation IIR HEAT 

KAB-50Kr-M-FE 3rd Generation FRAG-HE 

KAB-50Kr-MT-FE 3rd Generation IIR FRAG-HE 

KAB-250Kr-M 3rd Generation HE 

KAB-250Kr-M-F-E 3rd Generation FRAG-HE 

KAB-250Kr-M-OD-E 3rd Generation FAE

KAB-500Kr-M 3rd Generation HE

KAB-500Kr-M-Pr-E 3rd Gen Bunker Buster 

KAB-500Kr-M-F-E 3rd Generation FRAG-HE 

KAB-500Kr-M-OD-E 3rd Generation FAE 

KAB-500Kr-M-K-E 3rd Gen Cluster Bomb


Satellite Guided Munitions 

Kh-25MS-M Satellite guided HE 

Kh-25MS-F Satellite guided FRAG-HE 

KAB-250S-E satellite guided HE bomb 

KAB-500S-E Satellite guided HE bomb 

KAB-500Kr UMPK Satellite guided TV bomb 

ZAB-100 UMPK satellite guided Incen bomb 

ZAB-250 UMPK satellite guided Incen bomb

ODAB-500 UMPK satellite guided FAE bomb 

RBK-500 UMPK satellite guided cluster bomb

FAB-250 UMPK satellite guided HE bomb 

FAB-500 UMPK satellite guided HE bomb 

FAB-250 UMPB satellite guided HE bomb 

FAB-500 UMPB satellite guided HE bomb 


Unguided Bombs 

FAB-250 Unguided HE Bomb 

FAB-500 Unguided HE Bomb 

OFAB-150 Unguided Frag Bomb 

OFAB-250 Unguided Frag Bomb 

OFAB-500 Unguided Frag Bomb 

PLAB-250-120 Unguided ASW bomb 

ZAB-100-105 Unguided Incendiary bomb

ZAB-250-200 Unguided Incendiary bomb 

ODAB-500 Unguided fuel air bomb 

PTAB-500 Unguided anti tank bomb 

PTAB-500Y Unguided Anti Tank bomb 


Rockets 

S-25L 2nd Generation laser guided rocket

S-25-OFM 1st Generation Bunker buster 

S-25-OF high explosive Rocket 

S-13B 1st Generation Bunker buster 

S-13T tandem HEAT AT round 

S-13OF AP Anti armour frag round 

S-13DF thermobaric round 

S-13Kor 2nd Generation laser guided rocket


GSh-30-1 

9-A1-4071K 30x165mm HEI

9-A1-4071K 30x165mm HE-T

9-A1-4071K 30x165mm AP-T

9-A1-4071K 30x165mm SAPHEI

9-A1-4071K 30x165mm MKETF


Cluster Munitions

KMGU-2 cluster Munition dispenser 


UB 



D model 







MiG-29 Fulcrum Family


MiG-29A 

Concept: 1973

Designed: 1975

Prototype 1977

Completed 1980

Production: 1982

Service 1985

Aircraft Role: Air Superiority 

Generation: 4th

Combat Rank: A

Number Made: 1400+


MiG-29AK

Designed: 1982

Prototype: 1988

Aircraft Role: MultiRole/Air Superiority 

Generation: 4th

Combat Rank: D

Number Made: 10+


MiG-29M

Designed: 1983

Prototype: 1986

Aircraft Role: MultiRole/Strike Fighter 

Generation: 4th

Combat Rank: D

Number Made: 20+


MiG-29M2

Designed: 1996

Prototype: 1997

Completed 2005

Production: 2009

Service: 2012

Aircraft Role: MultiRole/Strike Fighter  

Generation: 4+

Combat Rank: D

Number Made: 50+


MiG-29S 

Designed: 1985

Prototype 1988

Completed 1989

Production: 1990

Service: 1994

Aircraft Role: Air Superiority  

Generation: 4th

Combat Rank: A

Number Made: 50+


MiG-29SM

Designed: 1993

Prototype 1995

Completed 1996

Aircraft Role: MultiRole/Strike Fighter 

Generation: 4+

Combat Rank: A

Number Made: 10+


MiG-29SMT

Designed: 1995

Prototype: 1997

Completed: 1998

Production: 2004

Service: 2006

Aircraft Role: MultiRole/Strike Fighter 

Generation: 4+

Combat Rank: A

Number Made: 100+


MiG-29K

Designed: 1990

Prototype: 2002

Completed: 2005

Production: 2013

Service: 2015

Combat Rank: C

Generation: 4+

Aircraft Role: MultiRole/Strike Fighter

Number Made: 70+


Engine and Airframe: All metal construction with an RCS minimum of 5m². Crew of 1. Length: 17.3 m. Height: 4.7 m. Wingspan 11.3 m. Wing area 38 m². Frame weight 11,000 kg. Takeoff weight 18,000 kg. Max Fuel 3500 kg  2× Klimov RD-33 axial flow low bypass turbofans with an analogue electronic engine control with 98 kN of thrust and up to 162 kN in afterburner. 


(SMT, AK and M model can add 2× Klimov RD-33-3 axial flow low bypass turbofans with a digital electronic engine control with 100 kN of thrust and up to 164 kN in afterburner) 


(M2 model adds CAD composite construction Airframe with an RCS minimum of 5m². Crew of 2. Length 17.3 m. Height 4.4 m. Wingspan 12 m. Wing area 45 m². Frame weight 12,000 kg. Takeoff weight 26,000 kg. Max Fuel 4,500 kg. 2× Klimov RD-33MK axial flow high bypass FADEC turbofans with 102 kN of thrust and 172 kN of thrust in afterburner. Service Ceiling up to 18 km. Wing loading of 370-400 kg/m². Sustained G tolerance of 9g and an Overload Tolerance of 12g and wing break at 18-24g. Refueling boom)


(K model adds CAD composite construction LV Airframe with an RCS minimum of 1m². Crew of 1-2. Length 17.3 m. Height 4.4 m. Wingspan 12 m. Wing area 45 m². Frame weight 11,000 kg. Takeoff weight 24,000 kg. Max Fuel 4,500 kg. 2× Klimov RD-33MK axial flow high bypass FADEC turbofans with 102 kN of thrust and 172 kN of thrust in afterburner. Service Ceiling up to 18 km. Refueling boom)


Speed and Endurance: Top speed of mach 2 to 2.3 at 15 km+, mach 2 to 2.1 at 10 km+, mach 1.8 to 2 to at 5 km+ and mach 1 to 1.2 at sea level. Combat Range of 500 to 700 km. Service Ceiling up to 18-23 km. Acceleration 7-14 seconds to mach 1 at sea level. Stall speed 100-160 kph. Take off distance is 300m with ATA payload to 800m for full payload. Landing distance 500 to 700m


(K model adds Top speed of mach 2.1 to 2.4 at 15 km+, mach 2 to 2.3 at 10 km+, mach 1.9 to 2 to at 5 km+ and mach 1 to 1.2 at sea level. Combat range of 900-1100 km. Acceleration 8-13 seconds to mach 1 at sea level. Stall speed 90-120 kph. Take off distance is 300m with ATA payload to 700m for full payload. Landing distance 500 to 700m) 


Manuvarabilities: Thrust to weight ratio of 1 at full air to air payload and 1.4 at half fuel/loadout. Roll rate of 180 deg/s at high speed and 220 deg/s at low speed. Climb rate of 260-230 m/s. Angle of Attack at 22° at mach 2>, 35° at mach 1> and 48° at mach <1. 20 to 40 kph/s speed bleed at high g instantaneous maneuvers and 5 to 20 kph/s speed bleed at high g sustained maneuvers. Sustained G tolerance of 9g and an Overload Tolerance of 12g and wing break at 18g. Wing loading of 380-405 kg/m². 4× LERXs with pitch of ±40°.and 2× elevators with pitch of -30°. 


(K adds Thrust to weight ratio of 1.2 at full air to air payload and 1.4 at half fuel/loadout and 0.8 at full loadout. Roll rate of 200 deg/s at high speed and 360 deg/s at low speed. Climb rate of 300-350 m/s. Angle of Attack at 30° at mach 2>, 50° at mach 1> and 70° at mach <1. 10 to 40 kph/s speed bleed at high g instantaneous maneuvers and 5 to 15 kph/s speed bleed at high g sustained maneuvers. Wing loading of 370-400 kg/m². Sustained G tolerance of 9g and an Overload Tolerance of 12g and wing break at 18-24g. 2× LERXs with pitch of ±60°)


Aircraft Turn Rates 


Sustained turn rates 


Mach ~1.5 Speeds 

● 1-3 deg/s at 10 km altitude 

● 4-6 deg/s at 5 km altitude 

● 6-9 deg/s at sea level 


Mach ~1 Speeds 

● 7-8 deg/s at 10 km altitude 

● 9-12 deg/s at 5 km altitude 

● 13-16 deg/s at sea level 


Mach ~0.5 Speeds 

● 11-12 deg/s at 10 km altitude 

● 14-17 deg/s at 5 km altitude 

● 19-22 deg/s at sea level 


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 9-13 deg/s 


Mach ~1 Speeds 

● 19-22 deg/s 


Mach ~0.5 Speeds 

● 26-28 deg/s 


K and M2 model adds 


Sustained turn rates 


Mach ~1.5 Speeds 

● 2-3 deg/s at 10 km altitude 

● 4-6 deg/s at 5 km altitude 

● 7-10 deg/s at sea level   


Mach ~1 Speeds 

● 13-14 deg/s at 10 km altitude 

● 16-18 deg/s at 5 km altitude 

● 17-20 deg/s at sea level   


Mach ~0.5 Speeds 

● 13-15 deg/s at 10 km altitude 

● 16-19 deg/s at 5 km altitude 

● 20-24 deg/s at sea level   


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 4-5 deg/s at 10 km altitude 

● 6-8 deg/s at 5 km altitude 

● 9-12 deg/s at sea level  


Mach ~1 Speeds 

● 15-17 deg/s at 10 km altitude 

● 18-21 deg/s at 5 km altitude 

● 20-24 deg/s at sea level  


Mach ~0.5 Speeds 

● 23-25 deg/s at 10 km altitude 

● 26-30 deg/s at 5 km altitude 

● 30-35 deg/s at sea level  


Airframe RCS

RCS Minimum: 5m²

RCS Median: 6m²

RCS Average: 7-10m²


K model adds 

Stealth: low visibility airframe, leading edge trails and full RAM applied to engines front and sides. 

 

K model Airframe 

RCS Minimum: 1m²

RCS Median: 1.5m²

RCS Average: 2-5m²


Navigation & Flight Control: PrNK-29 computerised navigation suite with a SAU-451-02 3× axis computerised autopilot and a BU-29 hydroelectric AFCS utilising a SVS-2Ts-2 4x bit digital ADC with a 50-100k SLOC-OS with navigation systems, electronic flight control and autopilot link. SN-29 digital navigation system with a TsVU-M 4x bit digital navigation computer using an electromechanical INS with a gyrostabilized accelerometer with an accuracy of 0.7° in pitch and 0.9° yaw and 0.5° in heading with an error rate of 7 km/ph and velocity error rate of <5 m/s. ARK-19 solid state ADF. RV-20 solid state radar altimeter. PK-29 2nd Generation cockpit with 1× CRT MFD. RSDN-10 Skip-2 digital radio navigation system with DVOR and ILS with a position accuracy of 100-300m and angular accuracy of ±0.5°. ZSh-5 Flight Helmet. 


(AK and M model adds SOI-29 3rd Generation cockpit with 2× monochrome CRT MFDs. SAU-451-2 6× axis fully computerised autopilot. SDU-29 analogue fly by wire AFCS with a Ts-040-2 8x bit digital ADC. RSDN-20 Alpha digital radio navigation system with DVOR and ILS with a position accuracy of 20-90m and angular accuracy of ±0.1°)


(K adds PrNK-29K fully computerised navigation/attack suite with a SAU-451 6× axis computerised autopilot and a KSU-941 fully digital fly by wire AFCS utilising a 32x bit digital ADC with a LINS-100RS fully digital navigation system utilising a Sigma-95N 32x bit fully digital navigation computer using a fully digital INS utilising a ring laser gyroscope, digital tuning fork quartz INS and gyrostabilized accelerometer with an accuracy of 0.03° in pitch and yaw and 0.05° in heading with an error rate of 0.09 km/ph and velocity error rate of <0.5 m/s with a hybridised position accuracy of <10m. RSBN-85 Vstrecha fully digital radio navigation system with DVOR and ILS with a position accuracy of 10-20m and angular accuracy of ±0.01°. MFI-10-7 4th Generation cockpit with 3× FHD LCD MFDs and HOTAS control stick. ZSh-7AP Flight Helmet. ARK-25 digital ADF. RV-21 digital radar altimeter. A-737 GLONASS-M Global navigation satellite system with a max CEP of 2m and average CEP of <8m)


(SMT model adds PNS-29-R fully computerised navigation/attack suite with a SAU-451 6× axis computerised autopilot and a SDU-29M digital fly by wire AFCS utilising a 32x bit digital ADC with a LINS-100RS fully digital navigation system utilising a Sigma-95N 32x bit fully digital navigation computer using a fully digital INS utilising a ring laser gyroscope, digital tuning fork quartz INS and gyrostabilized accelerometer with an accuracy of 0.03° in pitch and yaw and 0.05° in heading with an error rate of 0.09 km/ph and velocity error rate of <0.5 m/s with a hybridised position accuracy of <10m. RSBN-85 Vstrecha fully digital radio navigation system with DVOR and ILS with a position accuracy of 10-20m and angular accuracy of ±0.01°. MFI-10-6M 4th Generation cockpit with 2× HD LCD MFDs and HOTAS control stick. ZSh-7AP Flight Helmet. ARK-25 digital ADF. RV-21 digital radar altimeter. A-737 GLONASS-M Global navigation satellite system with a max CEP of 2m and average CEP of 10m)


Communication & C2: R-862/R-800 VHF/UHF and R-864 HF digital radios with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding and digital data encryption with text and voice formats utilised operating on 20 channels with data transfer speeds of 1.2 kbit/s, 10 kbit/s and 16 kbit/s with an operating communication range of 350 km with an integrated LChM FHSS system utilising up to 100 frequency hops per second and VChP CRNG encoding system with 10 rounds for 56 bit and 8 rounds for 96 bit. Rubezh-M digital GCI complex with the Spektr-1 and Biryusa digital navigation data links and BAN-75, SVPK, SPK-75 and SPK-68 digital command data links connected to the SAU-451 computerised autopilot, ARK-20 solid state ADF, SO-69 solid state IFF interrogator and SRZO-2P solid state IFF transponder linked to the PVO NDCC air defence network with fully automated ground controlled interception, weapons management, IFF integration, digital data encryption and navigation data utilising ground based computer and radar generated data exchange with pre recorded voice and text formats used with data transfer speeds of 45 bit/s, 80 bit/s and 96 bit/s every 5 to 10 seconds operating on 2 MHz to 400 MHz with up to 1000 frequency hops per second on 10 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1000 km with data exchange between up to 36 aircraft.


(12A models use KN-23 solid state navigation system, RV-4M radar altimeter, no RSDN-20 and no R-864, 12B models used further downgraded navigation system with RSBN-6S)


(M2, K, SM and SMT adds S-103 fully digital unified communication complex with an R-833 fully digital software defined VHF/UHF and HF radio with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding, rekeying encryption and full digital data encryption with text, image and voice formats utilised operating on 8 programmable channels and 256 frequency carriers with data transfer speeds of 16 kbit/s, 5 mbit/s and 11 mbit/s utilising an PPCh integrated FHSS and CRNG system utilising up to 1000 frequency hops per second and 7 round cryptographic encryption for 128 bit, 9 round cryptographic encryption for 192 bit and 10 round cryptographic encryption for 256 bit with an operating LOS communication range of 450 km and BLOS up to 5000 km with satellite link and the TCS-2M fully digital Tactical Data Link linked to NDMC NTsUO military command center utilising the YeESU-TZ military C4 network that organises coordination between the Voiska PVO-PRO air defence network and the PTK blue force tracking network with links to Andromeda-D, Akatsiya-E, Barnaul-T, Baikal-1ME, Universal-1E, Fundament-M and Polyana-D4M1 C2 softwares and Type-1B, Planet and VIP-117M3 data terminals with fully automated VOR, GCI and ILS with fully digital electronics, frequency hopping, ECM resistance, two way communication, navigation data, fully digital data encryption, multi aircraft link, multi platform subscription, weapons management, IFF integration, electronic countermeasure support and C4 integration utilising ground and air based computer and radar generated data exchange with pre recorded voice, text and image formats used, with data transfer speeds of 1024 bit/s, 1200 bit/s, 2.4 kbit/s, 4.8 kbit/s and 16 kbit/s every 1 to 2 seconds operating on 3 MHz to 300 MHz with up to 20,000 frequency hops per second on 26 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1500 km with data exchange between up to 20 subscribers. BTsVM-900 fully digital FMC utilising i486DX4-90 32x bit CPUs performing 2-3b IPS and 90-120b FLOPS using the RelMK32 1-2m SLOC RTOS using a BTsK-29 C2IS suite linked to the YeESU-TZ military C4 network with squads level blue force tracking, SATCOM integration, electronic countermeasure support, precision targeting, integrated aircraft health management software, digital navigation software, moving map display and data sharing) 


Fire Control: SUO-29 computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with digital sensors with stability augmentation with Sapfir-29 digital radar targeting and OEPS-29 infrared tracking and laser targeting with a Ts-100 digital FCC utilising 580VM80 8x bit CPUs performing 170-200k IPS and 20-30m FLOPS. N019 Rubin 3rd Generation Radar with an X band mechanically steered solid state long chord twist cassegrain antenna array using analogue to digital signal processing, coherent doppler filtering based LDSD and pulse doppler IFF integration with CW illumination for SARH guidance, reduced false alarm rates, BIST system and computerised radar image displayed with multi-mode operation, predictive flight path and non tracked target tracking functions and raster, conical, sector, circular and spiral scan scanning modes utilising SRC/LDSD, STTR, MTTR and HMD, LDR, IRST and RFR based ACMs air to air radar modes with gain modulation, notch filtering, polarization filtering and pulse compression ECCM with HPRF power output on average being 1 kW with a 6 kW max output with 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance and 1 channel for sidelobe suppression and ECM with a noise factor of 6 dB with a 700 mm antenna diameter. OLS-K 2nd Generation IRST with a LN² cooled conical scanning PbSe detector with an integrated 1.06 μm Nd:YAG laser rangefinder. ZSh-5 Helmet with Shchel-3UM 1st Generation HMD. ILS-31 4th Generation HUD with a digital LED glass display utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with an integrated digital bombing complex utilising gun, bomb and rocket CCRP and CCIP with gun EEGS. IPV 4th Generation Radar display with an SVD system utilising a polychrome raster image displayed on a CRT MFD with computerised target generation, ECM resolution, navigation data and aircraft flight information with data link integration. TsVB-29 digital ballistic computer utilising a 580VM80 8x bit CPU enabling gun and missile coursing.


(12A export models used Sapfir-29E pulse doppler radar with basic LDSD and reduced ECCM inferior SNP mode and no pulse doppler IFF, export OLS-29E with no laser rangefinder and no all aspect tracking, no HMD and no ECM System, 12B export models also removed OLS-29, latest ASP-17 series of HUD given, Sapfir-29EB with 2× target SNP and 4x bit Ts-100-02-06 FCC with SVD radar system removed) 


(M/AK model adds SUV-29M computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with digital sensors with stability augmentation with OEPrNK-29 data fusion system utilising NAV, IFF, RDR and EOT with Ts-400 digital FCC utilising L1839VM1 32x bit CPUs performing 700-900k IPS and 500-700m FLOPS. N010 Zhuk 4th Generation X band mechanically steered digital slotted planar antenna array with programmable digital signal processing, coherent doppler filtering and signal modulation based LDSD with missile & tactical data link and pulse doppler IFF and tactical & missile data link integration with CW illumination for SARH guidance, low false alarm rates and computerised radar image displaying with multi-mode operation, radar map freezing, raid assessment, predictive flight path, non tracked target tracking, BIST system, air and ground based JEM non cooperative target recognition functions and raster, conical, sector, circular and spiral scan scanning modes utilising SAR, RBGM, GTD, TAR and TFR air to ground radar modes and SRC/LDSD, MR, STTR, MTTR and HMD, LDR, IRST, EOT and multi target RFR based ACMs air to air radar modes with gain modulation, notch filtering, polarization filtering, low sidelobe antenna, and pulse compression ECCM with HPRF power output on average being 1.5 kW with 6 kW max output with 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance and 1 channel for sidelobe suppression and ECM with a noise factor of 4 dB with a 624 mm antenna diameter. TsVB-29BM digital ballistic computer utilising a KM1810VM88 16x bit CPU enabling automatic digital target lead and gun and missile coursing with gun, rocket and bomb CCRP and CCIP with a max bomb and rocket accuracy of <10-20m CEP at a range up to 2000m and altitudes up to 3000m and <100-300m CEP at a range up to 10,000m and altitude up to 10,000m. OLS-M multi-channel digital EOTS with a HD resolution TV sight with a ~720p day time image resolution, 1.06 μm Nd:YAG laser targeting system with laser rangefinding, laser designation and laser spot tracking and a 2nd Generation IRST & 1st Generation FLIR system utilising a LN² cooled infrared imaging InSb detector with an FPA format of 256x and a thermal image resolution of 384×288p) 


(S models onwards add RSDN-20 Alpha digital radio navigation system with DVOR and ILS with a position accuracy of 20-90m and angular accuracy of ±0.1°. N019M Topaz 3rd Generation Radar with an X band mechanically steered solid state long chord twist cassegrain antenna array using analogue to digital signal processing, coherent doppler filtering based LDSD with missile data link and pulse doppler IFF integration with CW illumination for SARH guidance, reduced false alarm rates, BIST system and computerised radar image displaying with multi-mode operation, predictive flight path and non tracked target tracking functions and raster, conical, sector, circular and spiral scan scanning modes utilising SRC/LDSD, STTR, MTTR and HMD, LDR, IRST and RFR based ACMs air to air radar modes with gain modulation, notch filtering, polarization filtering and pulse compression ECCM with HPRF power output on average being 1.5 kW with a 6 kW max output with 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance and 1 channel for sidelobe suppression and ECM with a noise factor of 6 dB with a 700 mm antenna diameter using a Ts-101 digital FCC utilising K1801 16x bit CPUs performing 300-400k IPS and 150-200m FLOPS) 


(SM model adds SUO-29SM computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with digital sensors with stability augmentation with OEPrNK-29 data fusion system utilising IFF, NAV, RDR, IRST, EOT and TDL displayed on one screen Sapfir-29SM radar targeting and OEPS-29SM electro optical, laser and infrared imaging/tracking targeting utilising a MVK-04 fully digital FCC with KOMDIV-32 32x bit CPUs performing 1-2b IPS and 5-8b FLOPS. N019MP Topaz-MP 3++ Generation X band mechanically steered solid state long chord twist cassegrain antenna array using programmable analogue to digital signal processing, coherent doppler filtering based LDSD with missile data link and pulse doppler IFF integration with CW illumination for SARH guidance, reduced false alarm rates, BIST system and computerised radar image displaying with multi-mode operation, predictive flight path and non tracked target tracking functions and raster, conical, sector, circular and spiral scan scanning modes utilising SRC/LDSD, STTR, MTTR and HMD, LDR, IRST and RFR based ACMs air to air radar modes and GTD, GTT and SAR air to ground radar modes with gain modulation, notch filtering, polarization filtering and pulse compression ECCM. TsVB-29SM digital ballistic computer utilising a KN1801VM3 16x bit CPU enabling automatic digital target lead and gun and missile coursing with gun, rocket and bomb CCRP and CCIP with a max bomb and rocket accuracy of <10-20m CEP at a range up to 2000m and altitudes up to 3000m and <100-300m CEP at a range up to 10,000m and altitude up to 10,000m. MFD-54 3rd Generation cockpit with 1× HD resolution LCD MFD and HOTAS control stick. ZSh-7AP Helmet with Shchel-3UM1 1st Generation HMD)


(SMT model adds SUO-29SM-1R fully computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with fully digital sensors with full stability augmentation with OEPrNK-29 data fusion system utilising IFF, NAV, RDR, IRST, EOT and TDL information displayed on one screen and Kedr data fusion system with RFCM, IRCM, MAW, ESM, ECM and RHAWS information displayed on one screen N041R radar targeting and OLS-UE electro optical, laser and infrared imaging/tracking targeting utilising a BTsVM-436-2M fully digital FCC with KOMDIV-32 32x bit CPUs performing 1-2b IPS and 7-10b FLOPS. N010M Zhuk-M 4th Generation X band mechanically steered digital slotted planar antenna array using a data fused system with programmable digital signal processing, coherent doppler filtering and signal modulation based LDSD with missile & tactical data link and pulse doppler IFF and tactical & missile data link integration with CW illumination for SARH guidance, low false alarm rates and computerised radar image displaying with multi-mode operation, radar map freezing, raid assessment, predictive flight path, non tracked target tracking, BIST system, air and ground based JEM, RCS and HRRP non cooperative target recognition functions and raster, conical, sector, circular and spiral scan scanning modes utilising SAR, RBGM, GMTI, GTD, TAR and TFR air to ground radar modes and SRC/LDSD, MR, STTR, MTTR and HMD, LDR, IRST, EOT and multi target RFR based ACMs air to air radar modes with gain modulation, notch filtering, low sidelobe antenna, polarization filtering and pulse compression ECCM with HPRF power output on average being 1.5 kW with 6 kW max output with 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance and 1 channel for sidelobe suppression and ECM with a noise factor of 3 dB with a 624 mm antenna diameter. OLS-13SM multi-channel fully digital EOTS with a HD resolution TV sight with a ~720p day time image resolution, 1.06 μm Nd:YAG laser targeting system with laser rangefinding, laser designation and laser spot tracking and a 2nd Generation IRST & 2nd Generation FLIR system utilising a LN² cooled infrared imaging InSb detector with an FPA format of 96x4 and a thermal image resolution of 576×480p. ZSh-7AP Helmet with a a NSTs-T-04 1st Generation HMD. TsVB-29SM digital ballistic computer utilising a KN1801VM3 16x bit CPU enabling automatic digital target lead and gun and missile coursing with gun, rocket and bomb CCRP and CCIP with a max bomb and rocket accuracy of <10-20m CEP at a range up to 2000m and altitudes up to 3000m and <100-300m CEP at a range up to 10,000m and altitude up to 10,000m. 5th Generation Radar display with an SVD system utilising a high resolution full colour raster image displayed on a LCD MFD with computerised target generation, ECM resolution, navigation data and aircraft flight information with data link integration. ILS-31M 4th Generation HUD with a digital LED glass display utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with an integrated digital bombing complex utilising gun, bomb and rocket CCRP and CCIP with gun EEGS)


(K and M2 adds SUO-29K fully computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with fully digital sensors with full stability augmentation with RLPK-29K radar targeting and OLS-UE electro optical, laser and infrared imaging/tracking targeting utilising OEPrNK-29 data fusion system utilising IFF, NAV, RDR, IRST, EOT and TDL information displayed on one screen and Kedr data fusion system with RFCM, IRCM, MAW, ESM, ECM and RHAWS information displayed on one screen utilising a Baget-55-04 fully digital FCC with KOMDIV-32 32x bit CPUs performing 1-4b IPS and 10-15b FLOPS. N010M Zhuk-M2 4th Generation X band mechanically steered digital slotted planar antenna array using a data fused system with programmable digital signal processing, coherent doppler filtering and signal modulation based LDSD with missile & tactical data link and pulse doppler IFF and tactical & missile data link integration with CW illumination for SARH guidance, low false alarm rates and computerised radar image displaying with multi-mode operation, radar map freezing, raid assessment, predictive flight path, non tracked target tracking, BIST system, air and ground based JEM, RCS and HRRP non cooperative target recognition functions and raster, conical, sector, circular and spiral scan scanning modes utilising SAR, RBGM, GMTI, GTD, TAR and TFR air to ground radar modes and SRC/LDSD, MR, STTR, MTTR and HMD, LDR, IRST, EOT and multi target RFR based ACMs air to air radar modes with gain modulation, notch filtering, low sidelobe antenna, polarization filtering and pulse compression ECCM with HPRF power output on average being 1.5 kW with 6 kW max output with 3 receiving channels with 1 channel for tracking and searching, 1 channel for weapons guidance and 1 channel for sidelobe suppression and ECM with a noise factor of 3 dB with a 624 mm antenna diameter. IKSh-1M 5th Generation HUD with a fully digital LCD glass display utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with an integrated digital bombing complex utilising gun, bomb and rocket CCRP and CCIP with gun EEGS and a digital MFD with electro optical slaving, mission control, navigation systems and weapons functions. OLS-13SM multi-channel fully digital EOTS with a HD resolution TV sight with a ~720p day time image resolution, 1.06 μm Nd:YAG laser targeting system with laser rangefinding, laser designation and laser spot tracking and a 2nd Generation IRST & 2nd Generation FLIR system utilising a LN² cooled infrared imaging InSb detector with an FPA format of 96x4 and a thermal image resolution of 576×480p. Zsh-7AP Helmet with a NSTsI-KOS 2nd Generation HMD. 5th Generation Radar display with an SVD system utilising a high resolution full colour raster image displayed on a LCD MFD with computerised target generation, ECM resolution, navigation data and aircraft flight information with data link integration. TsVB-29K fully digital ballistic computer utilising a L1839VM1 32x bit CPU enabling fully automatic digital target lead and gun and missile coursing with gun, rocket and bomb CCRP and CCIP with a bomb and rocket accuracy of <4-7m CEP at a range up to 2000m and altitudes up to 5000m and <50-100m CEP at a range up to 10,000m and altitude up to 10,000m) 


Targeting: Rubin radar with a horizontal scan range of 130° and vertical scan range of -36°/+56° enabling tracking of up to 10 targets with a 150 km Rmax range, 90 km detection range for RCS of 3m² and 60 km track range for an aircraft with an RCS of 3m² with a LDSD detection range of 15-35 km for 3m² and a LDSD track range of 13-25 km for an aircraft with an RCS of 3m² with a rangefinding radar gun engagement range up to 10 km with a tracking scan range of 80° in azimuth and ±8.2° in elevation and a scan time of 2.5 to 5 seconds with max tracking target velocity at over 2500 kph and stores tracking information for up to 2 non tracked target with predictive flight paths for non tracked targets up to 10 seconds with LDSD ground clutter rejection of 60> dB and low chaff rejection with a MTBF of 40 to 60 hours. OLS-K IRST with single target tracking and automatic target track with an angular resolution of 0.1° and max tracking rate of 30 deg/s enabling a max range up to 90 km with a 50 to 80 km detection range 20 to 30 km rear track range with 15 km front track range for fighter sized targets and laser targeting system with laser rangefinding with an accuracy of 10m and a 8 km engagement range for aircraft with a horizontal FOV up to 60° and a vertical FOV of -15°/+60°. Shchel-3UM HMD with a 120° horizontal FOV and ±30° vertical FOV utilising automatic cueing for targeting with head tracking software.


(S models add Topaz radar with a horizontal scan range of 130° and vertical scan range of -36°/+56° enabling tracking of up to 10 targets and data linking of 2 missiles with a 150 km Rmax range, 100 km detection range for RCS of 3m² and 80 km track range for an aircraft with an RCS of 3m² with a LDSD detection range of 15-35 km for 3m² and a LDSD track range of 13-25 km for an aircraft with an RCS of 3m² with a rangefinding radar gun engagement range up to 10 km with a tracking scan range of 80° in azimuth and ±8.2° in elevation and a scan time of 2.5 to 5 seconds with max tracking target velocity at over 2500 kph and stores tracking information for up to 2 non tracked target with predictive flight paths for non tracked targets up to 10 seconds with LDSD ground clutter rejection of 60> dB and low chaff rejection with a MTBF of 40 to 60 hours)


(SM model adds Topaz-MP radar with a horizontal scan range of 130° and vertical scan range of -36°/+56° enabling tracking of up to 10 targets and data linking of 4 missiles with a 200 km Rmax range, 130 km detection range for RCS of 3m² and 90 km track range for an aircraft with an RCS of 3m² with a LDSD detection range of 50-70 km for 3m² and a LDSD track range of 40-50 km for an aircraft with an RCS of 3m² with a rangefinding radar gun engagement range up to 10 km with ground mapping up to 77 km, with base image resolutions of 5, 15, 30 and 60 m at a spatial resolution size of 15, 24, 50 and 77 km with radar imaging complete in 40 seconds with a tracking scan range of 80° in azimuth and ±8.2° in elevation and a scan time of 2.5 to 5 seconds with max tracking target velocity at over 2500 kph and stores tracking information for up to 4 non tracked target with predictive flight paths for non tracked targets up to 10 seconds with LDSD ground clutter rejection of 60> dB and low chaff rejection with a MTBF of 60 to 100 hours. OLS-13SM fully stabilised sight with a fully digital electro optical system with a 4× optical magnification with an FOV of 18.75° and a 10× optical magnification with an FOV of 7.5° with an independent stabilised vertical movement of -15°/+60° and independent stabilised horizontal movement of 180° with a moving stabilisation accuracy of ±0.1 mils in azimuth and elevation and minimum/maximum stabilised sight movements of 0.03/60 deg/s with an angular tracking rate of 10 to 30 deg/s with FLIR enabling a max range of 20 km, detection of tank sized targets up to 10 km and identification up to 2 km with detection of corvette sized warships up to 16 km with identification up to 10 km with detection of fighter sized targets up to 13 km and identification up to 2 km, TV sight enabling a max range of 15 km with detection of tank sized targets up to 8 km and identification up to 6 km with detection of fighter sized targets up to 10 km and identification up to 8 km with NFOV detection of corvette sized warships up to 13 km with identification up to 11 km, IRST with tracking of up to 2 targets and automatic target tracking with an angular resolution of 0.1° and max tracking rate of 120 deg/s enabling a max detection range up to 100 km with a 50 to 80 km detection range and 20 to 40 km rear track range with 15 km front track range for fighter sized targets and a 20 km track range for ground targets and laser targeting system with laser rangefinding, laser designation and laser spot tracking with an accuracy of 5m with with a 15 km engagement range for aircraft and 20 km engagement range for ground targets. Shchel-3UM1 HMD with a 140° horizontal FOV and -30°/+30° vertical FOV utilising automatic cueing for targeting with head tracking software)


(SMT adds Zhuk-M radar with a 170° horizontal and -40°/+56° vertical scan range enabling tracking of up to 14 targets and data linking of 4 missiles with a Rmax range up to 300 km, with a 150 km detection range for 16m² and 120 km track range for an aircraft with an RCS of 5m² with a LDSD detection range of 40-110 km for 5m² and a LDSD track range of 40-110 km for an aircraft with an RCS of 5m² with a rangefinding radar gun engagement range up to 10 km with a 300 km max ground detection range with a 25 km detection range for tank sized targets and 10 km track range with SAR imaging up to 80 km, with base image resolutions of 3, 30 and 300 m at a spatial resolution size of 20, 60 and 80 km with radar imaging complete in 40 seconds with a tracking scan range of 120° in azimuth and ±30° in elevation with a tracking scan sweep in 2 seconds with max tracking target velocity at over 3700 kph and stores tracking information for up to 10 non tracked targets with predictive flight paths for non tracked targets up to 12 seconds with LDSD ground clutter rejection of 70> dB, NCTR for 1 target up to 30 km with a scan range of ±15° in azimuth and ±5° in elevation with up to 20 preprogrammed target identifiers and high chaff rejection with a MTBF of 60 to 200 hours. OLS-13SM fully stabilised sight with a fully digital electro optical system with a 4× optical magnification with an FOV of 18.75° and a 10× optical magnification with an FOV of 7.5° with an independent stabilised vertical movement of -15°/+60° and independent stabilised horizontal movement of 180° with a moving stabilisation accuracy of ±0.1 mils in azimuth and elevation and minimum/maximum stabilised sight movements of 0.03/60 deg/s with an angular tracking rate of 10 to 30 deg/s with FLIR enabling a max range of 20 km, detection of tank sized targets up to 10 km and identification up to 2 km with detection of corvette sized warships up to 16 km with identification up to 10 km with detection of fighter sized targets up to 13 km and identification up to 2 km, TV sight enabling a max range of 15 km with detection of tank sized targets up to 8 km and identification up to 6 km with detection of fighter sized targets up to 10 km and identification up to 8 km with NFOV detection of corvette sized warships up to 13 km with identification up to 11 km, IRST with tracking of up to 2 targets and automatic target tracking with an angular resolution of 0.1° and max tracking rate of 120 deg/s enabling a max detection range up to 100 km with a 50 to 80 km detection range and 20 to 40 km rear track range with 15 km front track range for fighter sized targets and a 20 km track range for ground targets and laser targeting system with laser rangefinding, laser designation and laser spot tracking with an accuracy of 5m with with a 15 km engagement range for aircraft and 20 km engagement range for ground targets.  NSTs-T-04 HMD with a 160° horizontal FOV and -40°/+40° vertical FOV utilising automatic cueing for targeting with head tracking software)


(M/AK model adds Zhuk radar with a 170° horizontal and -40°/+56° vertical scan range enabling tracking of up to 10 targets and data linking of 4 missiles with a Rmax range up to 200 km, with a 130 km detection range for 16m² and 100 km track range for an aircraft with an RCS of 5m² with a LDSD detection range of 30-100 km for 5m² and a LDSD track range of 20-60 km for an aircraft with an RCS of 5m² with a rangefinding radar gun engagement range up to 10 km with a 180 km max ground detection range with a 25 km detection range for tank sized targets and 10 km track range with a tracking scan range of 120° in azimuth and ±30° in elevation with a tracking scan sweep in 2 seconds with max tracking target velocity at over 3700 kph and stores tracking information for up to 10 non tracked targets with predictive flight paths for non tracked targets up to 12 seconds with LDSD ground clutter rejection of 70> dB and low chaff rejection with NCTR with up to 1 target up to 20 km with a scan range of ±15° in azimuth and ±5° in elevation with up to 20 preprogrammed target identifiers and high chaff rejection with a MTBF of 60 to 200 hours and OLS-M fully stabilised sight with a fully digital electro optical system with a 4× optical magnification with an FOV of 18.75° and a 10× optical magnification with an FOV of 7.5° with an independent stabilised vertical movement of -15°/+30° and independent stabilised horizontal movement of 120° with a moving stabilisation accuracy of ±0.2 mils in azimuth and elevation and minimum/maximum stabilised sight movements of 0.03/60 deg/s with an angular tracking rate of 10 to 20 deg/s with FLIR enabling a max range of 15 km, detection of tank sized targets up to 5 km and identification up to 2 km with detection of corvette sized warships up to 12 km with identification up to 7 km with detection of fighter sized targets up to 9 km and identification up to 2 km, TV sight enabling a max range of 15 km with detection of tank sized targets up to 8 km and identification up to 6 km with detection of fighter sized targets up to 10 km and identification up to 8 km with NFOV detection of corvette sized warships up to 13 km with identification up to 11 km, IRST with tracking of up to 2 targets and automatic target tracking with an angular resolution of 0.1° and max tracking rate of 120 deg/s enabling a max detection range up to 100 km with a 50 to 80 km detection range and 20 to 40 km rear track range with 15 km front track range for fighter sized targets and a 20 km track range for ground targets and laser targeting with laser rangefinding, laser designation and laser spot tracking with an accuracy of 10m with a 15 km engagement range for aircraft and 20 km engagement range for ground targets) 


(K and M2 adds Zhuk-M2 radar with a 170° horizontal and -40°/+56° vertical scan range enabling tracking of up to 20 targets and data linking of 4 missiles with a Rmax range up to 300 km, with a 150 km detection range for 16m² and 120 km track range for an aircraft with an RCS of 5m² with a LDSD detection range of 40-110 km for 5m² and a LDSD track range of 40-110 km for an aircraft with an RCS of 5m² with a rangefinding radar gun engagement range up to 10 km with a 300 km max ground detection range with a 25 km detection range for tank sized targets and 10 km track range with ground mapping up to 80 km, with base image resolutions of 3, 30 and 300 m at a spatial resolution size of 20, 60 and 80 km with radar imaging complete in 40 seconds with a tracking scan range of 120° in azimuth and ±30° in elevation with a tracking scan sweep in 2 seconds with max tracking target velocity at over 3700 kph and stores tracking information for up to 10 non tracked targets with predictive flight paths for non tracked targets up to 12 seconds with LDSD ground clutter rejection of 70> dB, NCTR with up to 1 target up to 30 km with a scan range of ±15° in azimuth and ±5° in elevation with up to 20 preprogrammed target identifiers and high chaff rejection with a MTBF of 200 to 300 hours. OLS-13SM fully stabilised sight with a fully digital electro optical system with a 4× optical magnification with an FOV of 18.75° and a 10× optical magnification with an FOV of 7.5° with an independent stabilised vertical movement of -15°/+60° and independent stabilised horizontal movement of 180° with a moving stabilisation accuracy of ±0.1 mils in azimuth and elevation and minimum/maximum stabilised sight movements of 0.03/60 deg/s with an angular tracking rate of 10 to 30 deg/s with FLIR enabling a max range of 20 km, detection of tank sized targets up to 10 km and identification up to 2 km with detection of corvette sized warships up to 16 km with identification up to 10 km with detection of fighter sized targets up to 13 km and identification up to 2 km, TV sight enabling a max range of 15 km with detection of tank sized targets up to 8 km and identification up to 6 km with detection of fighter sized targets up to 10 km and identification up to 8 km with NFOV detection of corvette sized warships up to 13 km with identification up to 11 km, IRST with tracking of up to 2 targets and automatic target tracking with an angular resolution of 0.1° and max tracking rate of 120 deg/s enabling a max detection range up to 100 km with a 50 to 80 km detection range and 20 to 40 km rear track range with 15 km front track range for fighter sized targets and a 20 km track range for ground targets and laser targeting system with laser rangefinding, laser designation and laser spot tracking with an accuracy of 5m with with a 15 km engagement range for aircraft and 20 km engagement range for ground targets. NSTsI-KOS HMD with a 180° horizontal FOV and ±40° vertical FOV utilising automatic cueing for targeting with navigation data and weapons management data displayed with head tracking) 


Targeting Pods for M/AK models 

APK-9 Tekon data link pod for live video feed of Kh-29 and Kh-59 seekers. 


K, SMT and M2 Targeting Pods 


M400 Sapsan 2nd Generation Targeting Pod with a FHD resolution TV sight with a ~1080p day time image resolution, Raduga-III 2nd Generation FLIR system utilising a 1PN99M matrix with a 576x2 FPA format, 768×576p thermal image resolution, 8-12 μm spectral range, pixel pitch of 30 μm, NETp of 70 mK and 50 Hz refresh rate and an Nd:YAG laser targeting system with laser rangefinding, laser designation and laser spot tracking with an accuracy of 10m with with a utilising a fully digital telescopic electro optical sight with a day time 4× optical magnification with an FOV of 18.5°, 30× optical magnification with a FOV of 2.5° and a 60× electro optical magnification with an FOV of 1.2° with a night time 1× optical magnification with an FOV of 18°, 8× optical magnification with a FOV of 2.2° and a 16× optical magnification with an FOV of 1.1° with independent stabilised depth movement, an independent stabilised vertical movement of -150°/+10° and independent stabilised horizontal movement of 180° with a moving stabilisation accuracy of ±0.1 in elevation and azimuth and minimum/ maximum stabilised sight movements of 0.02/60 deg/s with an angular tracking rate of 40 to 60 deg/s with tracking of up to 20 targets and locking of up to 4 with FLIR enabling a max range of 30 km, detection of tank sized targets up to 10 km and identification up to 2.5 km with detection of corvette sized warships up to 25 km with identification up to 17 km with detection of fighter sized targets up to 18 km and identification up to 3 km, TV sight enabling a max range of 60 km, detection of tank sized targets up to 42 km and identification up to 36 km with detection of corvette sized warships up to 57 km with identification up to 52 km with a 30 km laser engagement range for ground targets. 


Counter Measures: L-006M/SPO-15LM Beryoza-LM 2nd Generation digital RHAWS with 8 targets tracked with 6 preprogrammed threat identifiers and 5× receivers enabling a self protection envelope of 360° in azimuth and ±60° in elevation with band coverage of 4.4-10.3 GHz with a signal detectability range up to 225 km. SSP-2I digital fire countermeasure system. K-36DM Zero-Zero ejection seat. BVP-30-26 countermeasure dispenser utilising 1st Generation IRCM and RFCM with 60 total rounds using the PPR-26-13 composite aluminium chaff that activates in 0.3 seconds and creates a false target RCS of greater than 30m² and using the PPI-26 thermite based flare with a minimum burn time of 3 seconds. SO-69/SRZO-1P 2nd Generation solid state IFF interrogator / transponder linked to the Parol fully digital IFF system with aircraft ID, digital data encryption reprogramming and cryptographic encoding. P-591 digital ICAS. KKO-15LP digital full ECLSS. 


(12A/B models used SPO-15E Beryoza-E with no threat identification database or homing system and SO-57/SRZO-2 1st Generation analogue electronic IFF interrogator/transponder given, no ECM system)


(M and AK model adds L-150/SPO-32 Pastel 3rd Generation fully digital RHAWS with 16 targets tracked and 128> preprogrammed threat identifiers with guidance of up to 6 ARMs with 2 fired simultaneous and 10× receivers enabling a self protection envelope of 360° in azimuth and ±60° in elevation with band coverage of 1.2-18 GHz with a signal detectability range up to 320 km, SO-72/SRZO-2P 2nd Generation digital IFF interrogator/transponder linked to the Parol-2D fully digital IFF system with aircraft ID, full digital data encryption, radio/inertial navigation locating, reprogramming and cryptographic encoding, BVP-60-26 countermeasure dispenser utilising 1st Generation IRCM and 2nd Generation RFCM with 120 total rounds using the PPR-26-17 composite jammer assisted chaff that activates in 0.3 seconds and creates a false target RCS of greater than 30m² and using the PPI-26-1V thermite based flare with a minimum burn time of 3 seconds)


(K and M2 model adds L-150NU-29K/SPO-32M Pastel-M 4th Generation fully digital data fused RHAWS with 20 targets tracked with 242> preprogrammed threat identifiers with guidance of up to 8 ARMs with 4 fired simultaneous with 16× receivers enabling a self protection envelope of 360° in azimuth and ±180° in elevation with band coverage of 0.2-20 GHz with a signal detectability range up to 440 km. К-36D-35М zero-zero ejection seat. BVP-30-26M countermeasure dispenser utilising 2nd Generation IRCM and RFCM with 60 total rounds using the PPR-26-51 composite aluminium jammer assisted chaff that activates in 0.3 seconds and creates a false target RCS of greater than 60m² and using the PPI-26-2-1 spectral flare with a minimum burn time of 3 seconds. SO-96/SRZ-035M 3rd Generation fully digital IFF interrogator / transponder linked to the Parol-2D fully digital IFF system with aircraft ID, full digital data encryption, radio/inertial navigation locating, reprogramming and cryptographic encoding. KKO-15LP digital full ECLSS. Digital ICAS) 


(SM model adds adds SO-72/SRZO-2P 2nd Generation digital IFF interrogator / transponder linked to the Parol-2D fully digital IFF system with aircraft ID, full digital data encryption, radio/inertial navigation locating, reprogramming and cryptographic encoding. BVP-60-26 countermeasure dispenser utilising 1st Generation IRCM and 2nd Generation RFCM with 120 total rounds using the PPR-26-17 composite jammer assisted chaff that activates in 0.3 seconds and creates a false target RCS of greater than 30m² and using the PPI-26-1V thermite based flare with a minimum burn time of 3 seconds)


(SMT model adds L-150NU-29/SPO-32M Pastel-M 4th Generation fully digital data fused RHAWS with 20 targets tracked with 242> preprogrammed threat identifiers with guidance of up to 8 ARMs with 4 fired simultaneous with 16× receivers enabling a self protection envelope of 360° in azimuth and ±180° in elevation with band coverage of 0.2-20 GHz with a signal detectability range up to 440 km. SO-96/SRZ-035M 3rd Generation fully digital IFF interrogator / transponder linked to the Parol-2D fully digital IFF system with aircraft ID, full digital data encryption, radio/inertial navigation locating, reprogramming and cryptographic encoding. BVP-60-26 countermeasure dispenser utilising 1st Generation IRCM and 2nd Generation RFCM with 120 total rounds using the PPR-26-17 composite jammer assisted chaff that activates in 0.3 seconds and creates a false target RCS of greater than 30m² and using the PPI-26-1V thermite based flare with a minimum burn time of 3 seconds)


(From early 2020s onwards Parol-2D is replaced by Password-3 all digital IFF system with aircraft ID, low observability data sharing, satellite navigation locating, full digital data encryption, reprogramming and cryptographic encoding)


Electronic Warfare: L-203B Gardenyia-1FU 2nd Generation solid state SPJ with radio direction finding, monopulse countermeasure, continuous wave countermeasure and pulse doppler countermeasure ECCM with track breaker and blip enhancement ELINIT with 5× receivers enabling an ECCM protection envelope of 360° in azimuth with a self protection jamming range of 100 km>. 


(Early models had no ECM)


(SM, AK and M model adds L-203M Gardenyia-1FUM 3rd Generation digital SPJ utilising radio direction finder with AoA and PRF determination, monopulse countermeasure, continuous wave countermeasure, pulse doppler countermeasure, doppler shifting, home on jam and anti burn though ECCM with track breaker, decoy generation and blip enhancement ELINT with 8× receivers enabling an ECCM protection envelope of 360° in azimuth with a self protection jamming range of 200 km>)


(K, M2 and SMT model adds KS-418 Kedr 4th Generation fully digital SPJ suite utilising radio direction finder with AoA and PRF determination, simultaneous monopulse countermeasure, continuous wave countermeasure, pulse doppler countermeasure and LPIR countermeasure with doppler shifting, home on jam and anti burn though ECCM with track breaker, advanced decoy generation, blip enhancement and global navigation spoofing ELINT with 8× receivers enabling an ECCM protection envelope of 360° in azimuth with a self protection jamming range of 300 km> with MSP-418K 4th Generation fully digital active jamming system operating on 4-18 GHz with frequency agile deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, spot jamming, wave jamming, power managed jamming and DRFM jamming ECM with 2× GaAs AESA tapered slot antenna ECM transmitters enabling an active jamming range of 200 km>)


Active Jamming Pods 

SPS-161 Gardenia 2nd Generation solid state active jamming pod operating on 6-12 GHz with deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming and spot jamming ECM with track breaker and false target generation ELINIT with 2× planar spiral antenna ECM transmitters enabling an active jamming range of 200 km>. 


Active Jamming Pods for M, AK and S models

SPS-172 Smalta-PG 3rd Generation digital active jamming pod operating on 6-10 GHz with deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming and spot jamming ECM with track breaker and false target generation ELINIT with 2× PESA pyramidal horn ECM transmitters enabling an active jamming range of 200 km>. 


Guns: GSh-30-1 30mm autocannon with an integrated laser rangefinder slaved to radar with an effective firing range against aircraft up to 2 km.


Ordinance Capacity: 7x hardpoints with max 4000 kg munition capacity and 150 rounds for guns. 


(K, M, M2, S, SM, SMT and AK model adds 9× hardpoints with a max 5500 kg munition capacity with 150 rounds for gun) 


Common Air to Air Payloads 

● 4× APU-470 racks with R-27R 2× APU-73 racks with R-73 1× SPS-161

● 6× APU-470 racks with 4x R-27R and 2x R-27T 1× SPS-161 


R-27R

3rd Generation Radar Missile 

9B-1101 Inverse Monopulse X band Semi Active Seeker with a digital phase comparison antenna array with an INS utilising a radio correction data link with back up inertial operting guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a radio proximity fuse and back up impact detonation with a continuous rod warhead enabling a blast radius of 10-15 m²

~90 km max Range at 10 km+ altitude 

~70 km max Range at 5 km+ altitude 

~50 km max Range at sea level 

~30 km engagement range vs RCS of 5m² at sea level 

~50 km engagement range vs RCS of 5m² at 5 km+ altitude 

~70 km engagement range vs RCS of 5m² at 10 km+ altitude 

~10 km NEZ range vs RCS of 5m² at sea level 

~20 km NEZ range vs RCS of 5m² at 5 km> altitude

~30 km NEZ range vs RCS of 5m² at 10 km> altitude

~Mach 4 at 10 km+ altitude 

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Targeting Angles 35°

~Turn Rate 20 to 50 Deg/s

~Initial Acceleration of 210-370 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 74g 


R-27T 

4th Generation IR Missile 

Geofizika-36T LN² Cooled digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~70 km max Range at altitude 

~40 km max Range at sea level 

~60 km engagement range 

~All aspect lock range 5 km

~Rear aspect lock range 20 km

~Mach 4 at 10 km+ altitude 

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Rectile Speed: 125 Hz

~Flare rejection 0.6

~Gimbal limit: 55°

~Angular Tracking: 60 deg/s 

~Turn Rate 20 to 50 Deg/s

~Initial Acceleration of 210-370 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 74g 


R-73

4th Generation IR Missile 

Mayak-80 LN² Cooled digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~30 km max Range at 5 km> altitude 

~20 km max Range at sea level 

~20 km engagement range at 5 km>

~All aspect lock range 4 km

~Rear aspect lock range 10 km 

~Mach 3 at 5 km> altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.6

~Gimbal limit: 45°

~Angular Tracking: 60 deg/s 

~Turn Rate 90 to 120 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 60g 


GSh-30-1

9A-4071K 30×165mm SAPHEI


12A models used R-27TE with reduced angular Tracking, reduced off boresight and reduced Flare rejection and R-27RE with export Seeker with reduced engagement range whilst 12B models use R-60MKs for IR missiles


M, AK, S and SM model adds


Common Air to Air Payloads 

6× R-77 2× R-73M/R-27ET 1× SPS-172

6× R-27ER 2× R-73M/R-27ET 1× SPS-172


Common Air to Ground Payloads 

4× Kh-59 2× Kh-29 2× R-73M/R-27ET 1× SPS-172

4× KAB-500Kr 2× KAB-500L 2× R-73M/R-27ET 1× SPS-172

4× B-13L 2× S-24 2× R-73M/R-27ET 1× SPS-172


R-77

4th Generation Radar Missile 

9P-1348 Inverse Monopulse X band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a radio correction data link with back up inertial operting guidance, home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a Z23nA radio proximity fuse and back up impact detonation with with a high explosive blast warhead enabling a blast radius of 10-15 m²

~150 km max Range at 10 km+ altitude 

~120 km max Range at 5 km+ altitude 

~58 km max Range at sea level 

~35 km engagement range vs RCS of 5m² at sea level 

~80 km engagement range vs RCS of 5m² at 5 km+ altitude 

~110 km engagement range vs RCS of 5m² at 10 km+ altitude 

~15 km NEZ range vs RCS of 5m² at sea level 

~25 km NEZ range vs RCS of 5m² at 5 km> altitude

~30 km NEZ range vs RCS of 5m² at 10 km> altitude

~6 km ARH lock range vs RCS of 1m²

~18 km ARH lock range vs RCS of 5m²

~24 km ARH lock range vs RCS of 10m²

~0.1 m² minimum target RCS for ARH lock 

~Mach 4 at high altitude 

~Mach 3 at sea level 

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~50g Overload Tolerance 

~8g launch limiter

~10g target limiter 


R-27ER

3rd Generation Radar Missile 

9B-1101E Inverse Monopulse X band Semi Active Seeker with a fully digital phase comparison antenna array with an INS utilising a radio correction data link with back up IOG and polarisation filtering ECCM utilising a solid fuel rocket motor with a radio proximity fuse and back up impact detonation with a continuous rod warhead enabling a blast radius of 10-15 m²

~130 km max Range at 10 km+ altitude 

~110 km max Range at 5 km+ altitude 

~90 km max Range at sea level 

~70 km engagement range vs RCS of 5m² at sea level 

~90 km engagement range vs RCS of 5m² at 5 km+ altitude 

~110 km engagement range vs RCS of 5m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 5m² at sea level 

~30 km NEZ range vs RCS of 5m² at 5 km> altitude

~50 km NEZ range vs RCS of 5m² at 10 km> altitude

~Mach 5 at 10 km+ altitude 

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Targeting Angles 35°

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~60g Overload Tolerance 

~8g launch limiter 

~9g target limiter 


R-27ET 

4th Generation IR Missile 

Geofizika-36TE LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~120 km max Range at altitude 

~40 km max Range at sea level 

~80 km engagement range 

~All aspect lock range 20 km

~Rear aspect lock range 30 km

~Mach 4 at 10 km+ altitude 

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Rectile Speed: 125 Hz

~Flare rejection 0.6

~Gimbal limit: 55°

~Angular Tracking: 60 deg/s 

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 60g 


R-74

4th Generation IR Missile 

Mayak-80B LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~30 km max Range at 5 km> altitude 

~20 km max Range at sea level 

~20 km engagement range at 5 km> 

~All aspect lock range 6 km

~Rear aspect lock range 10 km

~Mach 3 at 5 km> altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.6

~TVC: Yes turns 180° / 3 seconds 

~Gimbal limit: 60°

~Angular Tracking: 60 deg/s 

~Turn Rate 90 to 120 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 60g 


M/AK model adds


Laser Guided Bombs 

KAB-500L 1st Generation LG HE  

KAB-500L-Pr-E 2nd Gen Bunker Buster 

KAB-500L-F-E 1st Generation FRAG-HE 

KAB-500L-OD-E 1st Generation FAE 

KAB-500L-K-E 1st Generation Cluster Bomb 


Optically Guided Bombs 

KAB-500Kr 2nd Generation HE

KAB-500Kr-Pr-E 2nd Gen Bunker Buster 

KAB-500Kr-F-E 2nd Generation FRAG-HE 

KAB-500Kr-OD-E 2nd Generation FAE 

KAB-500Kr-K-E 2nd Generation Cluster Bomb


Air to Ground Missiles 

Kh-59-M 3rd Generation HE Cruise Missile

Kh-59-K 3rd Generation HEAT Cruise Missile

Kh-59-KE 3rd Gen Cluster Cruise Missile

Kh-59L-M 2nd Gen Laser Guided HE

Kh-59L-K 2nd Gen Laser Guided HEAT

Kh-59L-KE 2nd Gen Laser Guided Cluster 

Kh-59T-M 2nd Generation OG HE

Kh-59T-K 2nd Generation OG HEAT

Kh-59T-KE 2nd Generation OG Cluster 

Kh-29T-M 2nd Generation OG HE

Kh-29T-K 2nd Generation OG HEAT 

Kh-29L-M 2nd Generation Laser Guided HE 

Kh-29L-K 2nd Generation Laser Guided HEAT 


Unguided Bombs 

FAB-500 HE bomb

FAB-250  HE bomb

BETAB-500 bunker buster

RBK-500 cluster munition bomb

RBK-250 cluster munition bomb

KMGU cluster munition dispenser 


Rockets 

S-13 KEP Rocket 

S-13T HEAT Rocket 

S-24 HE-FRAG 


SM model adds 


R-77-1A

4th Generation Radar Missile 

9B-1248 Inverse Monopulse X band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a bi-directional radio correction data link with back up inertial operting guidance, home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser and Z23nA radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~150 km max Range at 10 km+ altitude 

~120 km max Range at 5 km+ altitude 

~90 km max Range at sea level 

~50 km engagement range vs RCS of 5m² at sea level 

~90 km engagement range vs RCS of 5m² at 5 km+ altitude 

~120 km engagement range vs RCS of 5m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 5m² at sea level 

~30 km NEZ range vs RCS of 5m² at 5 km> altitude

~40 km NEZ range vs RCS of 5m² at 10 km> altitude

~6 km ARH lock range vs RCS of 1m²

~18 km ARH lock range vs RCS of 5m²

~24 km ARH lock range vs RCS of 10m²

~0.1 m² minimum target RCS for ARH lock 

~Mach 5 max target velocity 

~Mach 4 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~Launch limiter 9g 

~Target limiter 12g 

~Overload Tolerance 60g



M2, K and SMT models add 


Common Air to Air Payloads 

● 6× AKU-170 racks with R-77-1 2× APU-73 racks with R-74M 1× MSP-418K


Common Air to Ground Payloads 

2x O-25 2x B-13L 2x R-74M 1× MSP-418K

2x Kh-31AD 2x Kh-35U 1x Kh-61 2x R-74M 1× MSP-418K

3x Kh-58U 2x Kh-31PD 2x R-74M 1× MSP-418K

2x Kh-29D 4x Kh-29ML 2x R-74M 1× MSP-418K

2x Kh-59M2 4x KAB-500OD 2x R-74M 1× MSP-418K

2x KAB-1500Kr-OD 2x Kh-29D 2x R-74M 1× MSP-418K

1x Kh-59MKM 1x Kh-69 1x KAB-1500LG-Pr-E 1× MSP-418K


R-77-1B

4+ Generation Radar Missile 

9B-1103M-150 Inverse Monopulse X/Ku band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a bi-directional radio correction data link with back up inertial operting guidance, dual band, home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser and Z23nA radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~200 km max Range at 10 km+ altitude 

~150 km max Range at 5 km+ altitude 

~80 km max Range at sea level 

~50 km engagement range vs RCS of 5m² at sea level 

~110 km engagement range vs RCS of 5m² at 5 km+ altitude 

~140 km engagement range vs RCS of 5m² at 10 km+ altitude 

~30 km NEZ range vs RCS of 5m² at sea level 

~40 km NEZ range vs RCS of 5m² at 5 km> altitude

~60 km NEZ range vs RCS of 5m² at 10 km> altitude

~8 km ARH lock range vs RCS of 1m²

~20 km ARH lock range vs RCS of 5m²

~26 km ARH lock range vs RCS of 10m²

~0.05 m² minimum target RCS for ARH lock 

~Mach 5 max target velocity 

~Mach 4 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~Launch limiter 9g 

~Target limiter 12g 

~Overload Tolerance 60g


R-27ET 

4th Generation IR Missile 

Geofizika-36TE LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~120 km max Range at altitude 

~40 km max Range at sea level 

~80 km engagement range 

~All aspect lock range 20 km

~Rear aspect lock range 30 km

~Angular tracking 60 deg/s

~Mach 4 at 10 km+ altitude 

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Rectile Speed: 125 Hz

~Flare rejection 0.6

~Gimbal limit: 55°

~Angular Tracking: 60 deg/s 

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 60g 


R-74M

4+ Generation IR Missile 

Impuls-90 LN² Cooled NIR & UV channel fully digital pseudo-imaging HgCdTe Seeker with dual band, gatewidth and seeker shut off IRCCM

~50 km max Range at 5 km> altitude 

~40 km max Range at sea level 

~40 km engagement range at 5 km> altitude

~All aspect lock range 10 km

~Rear aspect lock range 10 km 

~Mach 3 at 5 km> altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.8

~Gimbal limit: 75°

~Angular Tracking: 60 deg/s 

~Turn Rate 120 to 180 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 80g 


Air to Ground Missiles  

Kh-69 LO 4th Gen Cluster Cruise Missile 

Kh-69 LO 4th Gen HEAT Cruise Missile 

Kh-59MK2-F-E LO 3rd Gen OG/IIR FRAG-HE 

Kh-59M2-M 2nd Generation OG HE 

Kh-59M2-K 2nd Generation OG HEAT 

Kh-59M2-KE 2nd Generation OG Cluster 

Kh-59M2D-M 2nd Generation OG/IIR HE 

Kh-59M2D-K 2nd Generation OG/IIR HEAT 

Kh-59M2D-KE 2nd Generation OG/IIR Cluster 

Kh-59MK-M 4th Generation HE Cruise Missile

Kh-59MK-K 4th Gen HEAT Cruise Missile

Kh-59MK-KE 4th Gen Cluster Cruise Missile

Kh-58UShKE 3rd Gen Anti Radiation  

Kh-58UShKE-TP 3rd Gen OG/IIR Anti Radiation

Kh-29MP-M 4th Gen HE Ballistic Missile 

Kh-29MP-K 4th Gen HEAT Ballistic Missile 

Kh-29TE-M 3rd Generation OG HE 

Kh-29TE-K 3rd Generation OG HEAT 

Kh-29TD-M 3rd Generation OG/IIR HE 

Kh-29TD-K 3rd Generation OG/IIR HEAT 

Kh-29ML-M 3rd Generation Laser Guided HE 

Kh-29ML-K 3rd Gen Laser Guided HEAT   


Bunker Busters 

Kh-59MKM 3rd Generation Bunker Buster 

Kh-59MK2-Pr LO 3rd Gen Bunker Buster 

KAB-500Kr-Pr-E 2nd Gen Bunker Buster 

KAB-500LG-Pr-E 2nd Gen Bunker Buster

KAB-250LG-Pr-E 2nd Generation Bunker Buster

BETAB-500SHP 1st Generation bunker buster

BETAB-500 1st Generation Bunker buster 

BETAB-500Y 1st Generation Bunker buster 


Laser Guided Bombs 

KAB-20LG-K 3rd Generation HEAT 

KAB-20LG-FE 3rd Generation FRAG-HE  

KAB-50LG-K 3rd Generation HEAT 

KAB-50LG-FE 3rd Generation FRAG-HE  

KAB-100LG-K 3rd Generation HEAT 

KAB-100LG-FE 3rd Generation FRAG-HE 

KAB-250LG 3rd Generation HE 

KAB-250LG-F-E 3rd Generation FRAG-HE 

KAB-250LG-OD-E 3rd Generation FAE

KAB-500MLG 3rd Generation HE

KAB-500MLG-Pr-E 3rd Gen Bunker Buster 

KAB-500MLG-F-E 3rd Generation FRAG-HE 

KAB-500MLG-OD-E 3rd Generation FAE 

KAB-500MLG-K-E 3rd Gen Cluster Bomb


Optically Guided Bombs 

KAB-500Kr 2nd Generation HE

KAB-500Kr-F-E 2nd Generation FRAG-HE 

KAB-500Kr-OD-E 2nd Generation FAE 

KAB-500Kr-K-E 2nd Generation Cluster Bomb


Satellite Guided Munitions 

Kh-25MS-M Satellite guided HE 

Kh-25MS-F Satellite guided FRAG-HE 

KAB-250S-E satellite guided HE bomb 

KAB-500S-E Satellite guided HE bomb 

KAB-500Kr UMPK Satellite guided TV bomb 

ZAB-100 UMPK satellite guided Incen bomb 

ZAB-250 UMPK satellite guided Incen bomb

ODAB-500 UMPK satellite guided FAE bomb 

RBK-500 UMPK satellite guided cluster bomb

FAB-250 UMPK satellite guided HE bomb 

FAB-500 UMPK satellite guided HE bomb 

FAB-250 UMPB satellite guided HE bomb 

FAB-500 UMPB satellite guided HE bomb 


Unguided Bombs 

FAB-250 Unguided HE Bomb 

FAB-500 Unguided HE Bomb 

OFAB-150 Unguided Frag Bomb 

OFAB-250 Unguided Frag Bomb 

OFAB-500 Unguided Frag Bomb 

PLAB-250-120 Unguided ASW bomb 

ZAB-100-105 Unguided Incendiary bomb

ZAB-250-200 Unguided Incendiary bomb 

ODAB-500 Unguided fuel air bomb 

PTAB-500 Unguided anti tank bomb 

PTAB-500Y Unguided Anti Tank bomb 


Rockets 

S-25L 2nd Generation laser guided rocket

S-25-OFM 1st Generation Bunker buster 

S-25-OF high explosive Rocket 

S-13B 1st Generation Bunker buster 

S-13T tandem HEAT AT round 

S-13OF AP Anti armour frag round 

S-13DF thermobaric round 

S-13Kor 2nd Generation laser guided rocket


GSh-30-1 

9-A1-4071K 30x165mm HEI

9-A1-4071K 30x165mm HE-T

9-A1-4071K 30x165mm AP-T

9-A1-4071K 30x165mm SAPHEI

9-A1-4071K 30x165mm MKETF


Cluster Munitions

KMGU-2 cluster Munition dispenser 


Later models add 


R-77-1C

4+ Generation Radar Missile 

9B-1103M-200PA Inverse Monopulse Ku band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a bi-directional radio correction data link with back up inertial operting guidance, home on jam, multimode guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser and Z23nA radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~200 km max Range at 10 km+ altitude 

~150 km max Range at 5 km+ altitude 

~80 km max Range at sea level 

~50 km engagement range vs RCS of 3m² at sea level 

~100 km engagement range vs RCS of 3m² at 5 km+ altitude 

~120 km engagement range vs RCS of 3m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 3m² at sea level 

~40 km NEZ range vs RCS of 3m² at 5 km> altitude

~60 km NEZ range vs RCS of 3m² at 10 km> altitude

~10 km ARH lock range vs RCS of 1m²

~20 km ARH lock range vs RCS of 3m²

~30 km ARH lock range vs RCS of 10m²

~0.05 m² minimum target RCS for ARH lock 

~Mach 5 max target velocity 

~Mach 4 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~Launch limiter 9g 

~Target limiter 12g 

~Overload Tolerance 60g


MiG-29 Prototype 


MiG-29A 


MiG-29S


MiG-29SM 

MiG-29SMT 

MiG-29M


MiG-29M2 


MiG-29AK


MiG-29K (prototype)

MiG-29K


2 seater K 






MiG-25/31 Fox Family 


MiG-25P 

Concept: 1959

Designed: 1961

Prototype: 1964

Completed: 1969

Production: 1970

Service: 1971

Generation: 3rd

Aircraft Role: Interceptor 

Combat Rank: S

Number Made: 500+


MiG-25PD

Designed: 1976

Prototype: 1976

Completed: 1978

Production: 1979

Service: 1980

Generation: 3+

Aircraft Role: Interceptor 

Combat Rank: D

Number Made: 400+


MiG-31 

Concept: 1968

Designed: 1972

Prototype: 1975

Completed: 1978

Production: 1979

Service: 1981

Aircraft Role: Interceptor

Generation: 4th

Combat Rank: C

Number Made: 500+


MiG-31M 

Designed: 1983

Prototype: 1985

Aircraft Role: Interceptor 

Generation: 4+

Combat Rank: D

Number Made: 8


MiG-31B

Prototype: 1988

Completed: 1989

Production: 1990

Service: 1992

Aircraft Role: Interceptor 

Generation: 4th

Combat Rank: B

Number Made: 400+


MiG-31BM

Prototype: 1998

Completed: 2009

Production: 2014

Service: 2019

Aircraft Role: Interdictor 

Generation: 4+

Combat Rank: S

Number Made: 150+


Engine and Airframe: All metal construction with an RCS minimum of 15m². Crew of 1. Length 14 m. Height 6.1 m. Wingspan 14 m. Wing area 61 m². Frame weight 20,000 kg. Takeoff weight 37,000 kg. Max Fuel 13,000 kg. 2× Tumansky R-15B-300 axial flow turbojets with an analogue electronic engine control with 148 kN of thrust and 200 kN in afterburner. 


(31 model adds All metal construction with an RCS minimum of 15m² Crew of 2. Length: 22 m. Height: 6.5 m. Wingspan 13.5 m. Wing area: 62 m². Frame weight 21,820 kg. Takeoff weight: 46,200 kg. Max Fuel: 16,130 kg. 2× Soloviev D-30F-6 axial flow low bypass turbofans with a digital electronic engine control with 186 kN of thrust and 304 kN in afterburner. Sustained G tolerance of 5g and an Overload Tolerance of 8g with wing break at 12g. Wing loading of 590-650 kg/m²) 


(B model adds in flight refueling) 


Speed and  Endurance: Top speed of mach 3 to 3.2 at 20 km+, mach 2.8 to 3 to at 10 km+ and mach 1 to 1.2 at sea level. Service Ceiling of 20 to 27 km. Combat range of 400-600 km. Acceleration 11-17 seconds to mach 1 at sea level. Stall speed 200-280 kph. 


(31 adds Top speed of mach 3 to 3.2 at 15 km+, mach 2.8 to 3 to at 10 km+ and mach 1.1 to 1.3 at sea level. Service Ceiling of 23 to 29 km. Combat Range of 700-1500 km. Acceleration 11-14 seconds at sea level. Stall speed 170-230 kph)


(31M and BM model adds 2× Soloviev D-30-F6M FADEC Turbofans with 192 kN of thrust and 312 kN in afterburner in afterburner with Top speed of mach 3 to 3.2> at 15 km+, mach 2.8 to 3 to at 10 km+ and mach 1.3 to 1.4 at sea level)


Manuvarabilities: Thrust to weight ratio of 0.4 at full air to air payload and 0.6 at half fuel/loadout. Roll rate of 200 deg/s at high speed and 220 deg/s at low speed. Climb rate of 260-230 m/s. Angle of Attack at 6° at mach 2>, 10° at mach 1> and 14° at mach <1. 100 to 300 kph/s speed bleed at high g instantaneous maneuvers and 30 to 150 kph/s speed bleed at high g sustained maneuvers. Wing loading of 590-630 kg/m². Sustained G tolerance of 5g and a max Overload Tolerance of 7g with wing break at 10.5g. 2× LERXs with pitch of ±20°.


(31 adds Thrust to weight ratio of 0.7 at full air to air payload and 0.9 at half fuel/loadout. Roll rate of 200 deg/s at high speed and 240 deg/s at low speed. Climb rate of 260-330 m/s. Angle of Attack at 10° at mach 2>, 15° at mach 1> and 20° at mach <1. 70 to 200 kph/s speed bleed at high g instantaneous maneuvers and 30 to 120 kph/s speed bleed at high g sustained maneuvers)


(31M model improves G tolerance to 7-9g)


Aircraft Turn Rates 


Sustained turn rates 


Mach ~1.5 Speeds 

● 1 deg/s at 5 km altitude 

● 1-3 deg/s at sea level 


Mach ~1 Speeds 

● 1-2 deg/s at 10 km altitude 

● 3-5 deg/s at 5 km altitude 

● 4-7 deg/s at sea level 


Mach ~0.5 Speeds 

● 3-5 deg/s at 10 km altitude 

● 5-8 deg/s at 5 km altitude 

● 8-12 deg/s at sea level 


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 3-5 deg/s 


Mach ~1 Speeds 

● 2-4 deg/s at 10 km altitude 

● 6-9 deg/s at 5 km altitude 

● 10-14 deg/s at sea level  


Mach ~0.5 Speeds 

● 6-9 deg/s at 10 km altitude 

● 10-14 deg/s at 5 km altitude 

● 13-18 deg/s at sea level  


31 models add 


Sustained turn rates 


Mach ~1.5 Speeds 

● 1 deg/s at 5 km altitude 

● 1-4 deg/s at sea level 


Mach ~1 Speeds 

● 3-4 deg/s at 10 km altitude 

● 4-6 deg/s at 5 km altitude 

● 6-9 deg/s at sea level 


Mach ~0.5 Speeds 

● 5-7 deg/s at 10 km altitude 

● 8-11 deg/s at 5 km altitude 

● 11-15 deg/s at sea level 


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 1-3 deg/s at 5 km altitude 

● 3-6 deg/s at sea level  


Mach ~1 Speeds 

● 3-6 deg/s at 10 km altitude 

● 7-11 deg/s at 5 km altitude 

● 8-13 deg/s at sea level  


Mach ~0.5 Speeds 

● 6-9 deg/s at 10 km altitude 

● 10-14 deg/s at 5 km altitude 

● 15-20 deg/s at sea level  


Airframe RCS

RCS Minimum: 15m²

RCS Median: 17m²

RCS Average: 20-25m²


Navigation & Flight Control: PrNK-155 analogue Navigation suite. BU-25 hydroelectric AFCS with SVSt2-155 nuvistor electronic ADC. 1st Generation cockpit. Polyot-11-25 analogue navigation system with an NVU-25 nuvistor navigation computer using a SKV-2N2 electromechanical INS with a gyrostabilized accelerometer with an accuracy of 0.7° in pitch and 0.9° yaw and 0.5° in heading with an error rate of 7 km/ph and velocity error rate of <5 m/s. ARK-10 analogue ADF, RSBN-5S Iskra-K analogue electronic radio navigation system with VOR with a position accuracy of 500-1200m and angular accuracy of ±4°. RV-4 analogue radar altimeter with SAU-155P1 3× axis electromechanical autopilot. ZSh-3 Flight Helmet. 


(31 adds PrNK-31 computerised navigation suite with a SAU-155МP 3× axis computerised autopilot and a SUU-25MP Electro hydraulic AFCS utilising a Ts-080 16x bit digital ADC with a 100-200k SLOC-OS with navigation systems, electronic flight control and autopilot link. KN-25 digital navigation system utilising a Ts-050 8x bit digital navigation computer using IP-1-72A/IS-1-72A digital INS with a digital tuning fork quartz and gyrostabilized accelerometer with an accuracy of 0.1° in pitch and yaw and 0.2° in heading with an error rate of 3.5 km/ph and velocity error rate of <3 m/s. ARK-19 solid state ADF. RV-15 solid state radar altimeter. RSDN-20 Alpha digital radio navigation system with DVOR and ILS with a position accuracy of 20-90m and angular accuracy of ±0.1°. 2nd Generation cockpit with 3× polychrome CRT MFDs. ZSh-5 Flight Helmet) 


(31BM adds PrNK-31BM fully computerised navigation suite with a SAU-155P1 6× axis computerised autopilot and a SUU-31 Electro hydraulic AFCS utilising a Ts-080 16x bit digital ADC with a TsPNK-31 fully digital navigation system with a Ts-061K 32x bit fully digital navigation computer using a fully digital INS utilising a ring laser gyroscope and gyrostabilized accelerometer with an accuracy of 0.04° in pitch and yaw and 0.07° in heading with an error rate of 1.3 km/ph and velocity error rate of <1 m/s with a hybridised position accuracy of <30m. ARK-19 solid state ADF. RV-15 solid state radar altimeter. RSDN-20 Alpha digital radio navigation system with DVOR and ILS with a position accuracy of 20-90m and angular accuracy of ±0.1°. MFI-68 4th Generation cockpit with 3× FHD resolution LCD MFDs with a HOTAS control stick. A-737 GLONASS-M Global navigation satellite system with a max CEP of 2m and average CEP of 10m. ZSh-7AP Flight Helmet) 


Fire Control: S-155 electromechanical FCS with angle of slide, angle of attack, air speed, altitude and aircraft position computed with analogue systems with the RLPK-25 radar targeting system. RP-25 Smerch-A1 2+ Generation mechanically steered J/I band analogue electronic monopulse radar system with a C band beacon interrogator with a long chord twist cassegrain antenna array with analogue signal processing and P, K, E and C scope radar image displayed with CW illumination for SARH guidance and IFF integration with multi mode operating function and raster, conical, and spiral scan scanning modes utilising SRC and STTR air to air radar modes with gain modulation, high power transmission and polarization filtering ECCM with LPRF power output on average being 200-400 W with a 700 kW max output with a 1000 mm antenna diameter. ITO-1 3rd Generation Radar display with a CRT screen utilising a K/E oscilloscope for target engagement and a P/C oscilloscope for target search. AVM-25 electromechanical ballistic computer enabling missile coursing.


(31 adds SBI-16 computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with digital sensors with stability augmentation with the OEPrNK-155MP data fusion system utilising RDR, IDL, IFF and IRST information displayed on one screen and the S-800 radar targeting and STP infrared tracking targeting system with an Argon-15K digital FCC utilising M1810VM86 16x bit CPUs performing 400-500k IPS and 250-300m FLOPS. N007 Zaslon 3+ Generation digital electronically steered X band PESA radar with an L band beacon interrogator with a slotted planar antenna array using digital signal processing with coherent doppler filtering and signal modulation based LDSD with missile & tactical data link and IFF integration with CW illumination for SARH guidance, low false alarm rates, BIST system and computerised radar image displayed with multi-mode operation, simultaneous searching tracking and guidance, predictive flight path and non tracked target tracking functions with raster, conical, sector, circular and spiral scan scanning modes utilising SRC/LDSD, STTR, MTTR and IRST and RFR based ACMs air to air radar modes with gain modulation, polarization filtering, sidelobe suppression, notch filtering, and pulse compression ECCM with 1700 total R/Es with a HPRF power output on average being 2.5 kW with a 10 kW max output with a 1100 mm antenna diameter. PPI-70V 4th Generation HUD with a digital LED glass display utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with gun EEGS. ITO-2 4th Generation Radar display with an SVD system utilising a polychrome raster image displayed on a CRT MFD with computerised target generation, ECM resolution, navigation data and aircraft flight information with data link integration. 8TK 1st Generation IRST utilising a LN² cooled conical scanning InSb detector. TsVB-155 digital ballistic computer utilising a 580VM80 8x bit CPU enabling gun and missile coursing)


(31M model added SBI-16M fully computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with digital sensors with stability augmentation with a Argon-A15KM1 fully digital FCC utilising L1839VM1 32x bit CPUs performing 30-50m IPS and 600-800m FLOPS, SUU-25MPM fully digital flight Control, SDU-25MP analogue fly by wire AFCS with a Ts-080 16x bit digital ADC, SAU-155МPM 6× axis computerised autopilot, SEI-31 3rd Generation cockpit with 4× polychrome CRT MFDs, N007M Zaslon-M 4th Generation electronically steered digital X band PESA radar system with an L band beacon interrogator with a slotted planar antenna array using a data fused system using programmable digital signal processing, coherent doppler filtering and signal modulation based LDSD with missile & tactical data link and pulse doppler IFF integration with CW illumination for SARH guidance, low false alarm rates and computerised radar image displayed with multi-mode operation, simultaneous searching tracking and guidance, predictive flight path, non tracked target tracking, raid assessment, predictive flight path, non tracked target tracking, BIST system and air based JAM non-cooperative target recognition functions and raster, conical, sector, circular and spiral scan scanning modes utilising SRC/LDSD, LPIR, STTR, MTTR and IRST and RFR based ACMs air to air radar modes with gain modulation, polarization filtering, sidelobe suppression, notch filtering, and pulse compression ECCM with 2,150 total R/Es with HPRF power output on average being 5 kW with a 400 kW max output with a 1400 mm antenna , PPI-90 5th Generation fully digital HUD with full gun EEGS and built in SVD radar scope, SNS-85 GLONASS Global navigation satellite system with a max CEP of 5m and average CEP of 30m and SB3541 fully digital FMC utilising MP1839 32x bit CPUs performing 15-30m IPS and 500-800m FLOPS with BTsK-31 RTOS with a 500-800k SLOC-OS with integrated aircraft health management software, electronic countermeasure support navigation software, moving map display and data sharing. TsPNK-31 fully digital navigation system with a Ts-061K 32x bit fully digital navigation computer using a fully digital INS utilising a ring laser gyroscope and gyrostabilized accelerometer with an accuracy of 0.04° in pitch and yaw and 0.07° in heading with an error rate of 1.3 km/ph and velocity error rate of <1 m/s with a hybridised position accuracy of <30m) 


(B model adds N007A Zaslon-A 3+ Generation digital electronically steered X band PESA radar with an L band beacon interrogator with a slotted planar antenna array using digital signal processing, coherent doppler filtering and signal modulation based LDSD with missile & tactical data link and pulse doppler IFF integration with CW illumination for SARH guidance, low false alarm rates, BIST system and computerised radar image displayed with multi-mode operation, simultaneous searching tracking and guidance, predictive flight path and non tracked target tracking functions and raster, conical, sector, circular and spiral scan scanning modes utilising SRC/LDSD, STTR, MTTR and IRST and RFR based ACMs air to air radar modes with gain modulation, polarization filtering, sidelobe suppression, notch filtering, and pulse compression ECCM with 1700 total R/E modules with a HPRF power output on average being 2.5 kW with a 10 kW max output with a 1100 mm antenna diameter)


(31BM adds SBI-16AM Barrier-M computerised IFFCS with temperature, pressure, angle of slide, angle of attack, air speed, altitude and aircraft position computed with digital sensors with stability augmentation with RLPK-31 radar targeting and STP infrared tracking targeting utilising with Baget-55-06 fully digital FCC utilising KOMDIV-64 64x bit 2× core CPUs CPUs performing 8-10b IPS and 90-150b FLOPS. N007AM Zaslon-AM 4th Generation electronically steered digital X band PESA radar system with an L band beacon interrogator with a slotted planar antenna array using a data fused system using programmable digital signal processing, coherent doppler filtering and signal modulation based LDSD with missile & tactical data link and pulse doppler IFF integration with CW illumination for SARH guidance, low false alarm rates and computerised radar image displayed with multi-mode operation, simultaneous searching tracking and guidance, predictive flight path, non tracked target tracking, raid assessment, predictive flight path, non tracked target tracking, BIST system and air and ground based JEM, RCS and HRRP non cooperative target recognition functions and raster, conical, sector, circular and spiral scan scanning modes utilising SRC/LDSD, LPIR, STTR, MTTR and IRST and RFR based ACMs air to air radar modes and SAR, GTD, GTT, TAR, TFR and GMTI air to ground modes with gain modulation, polarization filtering, sidelobe suppression, notch filtering, and pulse compression ECCM with 1700 total aL R/E modules with a HPRF power output on average being 2.5 kW with a 10 kW max output with a 1100 mm antenna diameter. PPV-1 4th Generation HUD with gun EEGS. 4th Generation Radar display. TsVB-31BM digital ballistic computer utilising a 580VM80 8x bit CPU enabling automatic digital target lead and gun and missile coursing)


(Later BM models add Vitebsk IRCM, RFCM, RHAWS, ESM and ECM data fusion system with information displayed on one screen)


Communication & C2: Klyon analogue electronic communication complex with the RSIU-5V VHF analogue electronic radio with 2 way communication, FM and AM receiving and built in IAD with voice formats with 20 pre set channels with an operating communication range of 200 km. Vozdukh-1M analogue electronic GCI complex with the ARL-SM Lazour-M analogue electronic navigation and command Data Link connected with the SAU-155P1 electromechanical autopilot, ARK-14 analogue ADF, SO-63 solid state interrogator and SRZO-2M analogue electronic IFF transponder linked to the Voyska PVO Strany URAGAN air defence network with fully automated ground controlled interception, data encryption and IFF integration utilising ground and air based radar and computer generated data exchange with pre recorded sound and text formats used, with data transfer speeds of 54 bit/s every 4 to 5 enabling a LOS data transmission range up to 350 km with data exchange between 3 aircraft. 


(The PD model adds SAU-155PD 3× axis electromechanical autopilot. KN-25 digital navigation system. RV-UM altimeter, Evkalipt solid state communication system with the R-855/R-832 VHF/UHF and R-802 HF solid state radios with 2 way communication, FM and AM receiving, built in IAD and secure voice encryption with voice formats utilised operating on 120 pre set channels with an operating communication range of 300 km. N005 Sapfir-25 2++ Generation J/X band mechanically steered solid state long chord twist cassegrain antenna arrays with a C band beacon interrogator with analogue to digital signal processing, BIST system and P, K, E and C scope radar image displayed with MTI based LDSD, CW illumination for SARH guidance and IFF integration with multi mode operating function and raster, conical, and spiral scan scanning modes utilising SRC/LDSD, MTTR, STTR and IRST based ACM air to air radar modes with high power transmission, gain modulation and polarization filtering ECCM with LPRF power output on average being 200-400 W with a 700 kW max output with a 1000 mm antenna diameter with an Argon-15 digital FCC utilising UB880D 8x bit CPUs performing 170-200k IPS and 20-30m FLOPS. TP-26Sh1 1st Generation IRST utilising a LN² cooled conical scanning InSb detector. R-855/R-832 VHF/UHF and R-802 HF solid state radios with 2 way communication, FM and AM receiving, built in IAD and secure voice encryption with voice formats utilised operating on 4 pre set channels with an operating communication range of 300 km. Rubezh digital GCI complex with the Biryusa digital navigation data links and BAN-75, SVPK, SPK-75 and SPK-68 digital command data links connected to the SAU-155P1 autopilot, ARK-19 solid state ADF, SO-69 solid state IFF interrogator and SRZO-2P solid state IFF transponder linked to the PVO NDCC air defence network with fully automated ground controlled interception, weapons management, IFF integration, digital data encryption and navigation data utilising ground based computer and radar generated data exchange with pre recorded voice and text formats used with data transfer speeds of 45 bit/s, 80 bit/s and 96 bit/s every 5 to 10 seconds operating on 2 MHz to 400 MHz with up to 1000 frequency hops per second on 10 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1000 km with data exchange between up to 36 aircraft)


(31 adds K-DlUE digital unified communication complex with R-862/R-800 VHF/UHF and R-864 HF digital radio with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding and digital data encryption with text and voice formats utilised operating on 20 channels with data transfer speeds of 1.2 kbit/s, 10 kbit/s and 16 kbit/s with an operating communication range of 350 km with an integrated LChM FHSS system utilising up to 100 frequency hops per second and VChP CRNG encoding system with 10 round cryptographic encryption for 56 bit and 8 round cryptographic encryption for 96 bit and the APD-518 digital information data link and RK-RLDN digital navigation data link linked to the Voyska PVO NDCC C2 air defence network with digital electronics, frequency hopping, ECM resistance, two way communication, digital data encryption, multi aircraft link, IFF integration, electronic countermeasure support and C2 integration utilising ground and air based computer and radar generated data exchange with pre recorded voice, text and image formats used, with data transfer speeds of 900 bit/s and 1000 bit/s every 2 to 4 seconds operating on 2 MHz to 400 MHz with up to 1000 frequency hops per second on 5 frequency carriers with LOS data transmission range up to 200 km and BLOS up to 2000 km with data exchange between up to 4 aircraft. Rubezh-M digital GCI complex with the Spektr-1 and Biryusa digital navigation data links and BAN-75, SVPK, SPK-75 and SPK-68 digital command data links connected to the SAU-155МP computerised autopilot, ARK-19 solid state ADF, SO-69 solid state IFF interrogator and SRZO-2P solid state IFF transponder linked to the PVO NDCC air defence network with fully automated ground controlled interception, weapons management, IFF integration, digital data encryption and navigation data utilising ground based computer and radar generated data exchange with pre recorded voice and text formats used with data transfer speeds of 45 bit/s, 80 bit/s and 96 bit/s every 5 to 10 seconds operating on 2 MHz to 400 MHz with up to 1000 frequency hops per second on 10 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1000 km with data exchange between up to 36 aircraft)


(31BM adds S-103 fully digital unified communication complex with an R-833 fully digital software defined VHF/UHF and HF radio with 2 way communication, FM and AM receiving, built in IAD, satellite communications, adaptive communication, multi channel communication, amplitude modulation, frequency hopping, cryptographic encoding, rekeying encryption and full digital data encryption with text, image and voice formats utilised operating on 8 programmable channels and 256 frequency carriers with data transfer speeds of 16 kbit/s, 5 mbit/s and 11 mbit/s utilising an PPCh integrated FHSS and CRNG system utilising up to 1000 frequency hops per second and 7 round cryptographic encryption for 128 bit, 9 round cryptographic encryption for 192 bit and 10 round cryptographic encryption for 256 bit with an operating LOS communication range of 450 km and BLOS up to 5000 km with satellite link and the TCS-2M fully digital Tactical Data Link linked to NDMC NTsUO military command center utilising the YeESU-TZ military C4 network that organises coordination between the Voiska PVO-PRO air defence network and the PTK blue force tracking network with links to Andromeda-D, Akatsiya-E, Barnaul-T, Baikal-1ME, Universal-1E, Fundament-M and Polyana-D4M1 C2 softwares and Type-1B, Planet and VIP-117M3 data terminals with fully automated VOR, GCI and ILS with fully digital electronics, frequency hopping, ECM resistance, two way communication, navigation data, fully digital data encryption, multi aircraft link, multi platform subscription, weapons management, IFF integration, electronic countermeasure support and C4 integration utilising ground and air based computer and radar generated data exchange with pre recorded voice, text and image formats used, with data transfer speeds of 1024 bit/s, 1200 bit/s, 2.4 kbit/s, 4.8 kbit/s and 16 kbit/s every 1 to 2 seconds operating on 3 MHz to 300 MHz with up to 20,000 frequency hops per second on 26 frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1500 km with data exchange between up to 20 subscribers. BTsVM-900 fully digital FMC utilising i486DX4-90 32x bit CPUs performing 2-3b IPS and 90-120b FLOPS using the RelMK32 1-2m SLOC RTOS using a BTsK-31 C2IS suite linked to the YeESU-TZ military C4 network with squads level blue force tracking, SATCOM integration, electronic countermeasure support, precision targeting, integrated aircraft health management software, digital navigation software, moving map display and data sharing) 


Targeting: Smerch-A1 radar with a horizontal scan range of 140° and -10°/+30° vertical scan range enabling an Rmax range up to 120 km, with a detection range of 100 km for 16m² and a track range of 50 km for an aircraft with an RCS of 16m² with a tracking scan range of 30° in azimuth and ±6° in elevation with a scan sweep in 2 to 4 seconds with max tracking target velocity at over 3700 kph with very low chaff rejection with a MTBF of 10 to 30 hours. 


(1973+ models add Smerch-A2 radar with a horizontal scan range of 140° and -10°/+30° vertical scan range enabling an Rmax range up to 120 km, with a detection range of 105 km for 16m² and a track range of 70 km for an aircraft with an RCS of 16m² with a tracking scan range of 30° in azimuth and -7°/+7° in elevation with a scan sweep in 3 to 4 seconds with max tracking target velocity at over 3700 kph with very low chaff rejection with a MTBCF of 10 to 30 hours) 


(The PD model adds Sapfir-25 radar with a horizontal scan range of 114° and -42°/+52° vertical scan range enabling tracking of up to 2 targets with an Rmax range up to 120 km, with a detection range of 115 km for 16m² and a track range of 80 km for an aircraft with an RCS of 16m² with a LDSD detection range of 30 km for 16m² and a LDSD track range of 25 km for an aircraft with an RCS of 16m² with a tracking scan range of 30° in azimuth and -7°/+7° in elevation with a scan sweep in 2 to 4 seconds with max tracking target velocity at over 3700 kph with LDSD ground clutter rejection of 40> dB with very low chaff rejection with a MTBF of 10 to 40 hours. TP-26Sh1 IRST with single target tracking with an angular resolution of 0.5° and max tracking rate of 8 deg/s enabling a max range up to 70 km with a 30 to 60 km detection range 15 to 20 km rear track range with 6 km front track range for fighter sized targets with a horizontal FOV up to 60° and a vertical FOV of ±7°)


(Export PS models received Smerch-A3 radar with similar performance to Sapfir-25 without SNP mode and LDSD)


(31 adds Zaslon radar with a 120° primary horizontal scan range and -60°/+70° vertical scan range enabling tracking of up to 10 targets and data linking of 4 missiles with an Rmax range of 300 km, in 15-24° STTR narrow beam mode detection range is 200 to 250 km vs RCS of 5m², 100 to 150 km vs RCS of 1m² and 80 to 100 km vs RCS of 0.1m², normal detection range of 210 km for an aircraft with an RCS of 16m² and a track range of 120 to 180 km for an aircraft with an RCS of 3-16m² with a LDSD detection range of 120 km for 16m² and a LDSD track range of 80 km for an aircraft with an RCS of 3m² with a rangefinding radar gun engagement range up to 10 km with a tracking scan range of 120° in azimuth and -60°/+70° in elevation with a full scan sweep in 0.2 seconds with max tracking target velocity up to 6300 kph and stores tracking information for up to 4 non tracked targets with predictive flight paths for non tracked targets up to 10 seconds with LDSD ground clutter rejection of 80> dB with low chaff rejection with a MTBF of 60 to 100 hours. 8TK IRST with single target tracking with an angular resolution of 0.5° and max tracking rate of 8 deg/s enabling a max range up to 90 km with a 50 to 80 km detection range 20 to 30 km rear track range with 15 km front track range for fighter sized targets with a horizontal FOV up to 120° and a vertical FOV of -13°/+6°) 


(31M model adds Zaslon-M radar with a 120° primary horizontal scan range and -60°/+70° vertical scan range enabling tracking of up to 24 targets and data linking of 6 missiles with an Rmax range of 500 km, in 15-24° STTR narrow beam mode detection range is 400 to 450 km vs RCS of 5m², 200 to 250 km vs RCS of 1m² and 90 to 120 km vs RCS of 0.001m², normal detection range of 400 km for an aircraft with an RCS of 16m² and a track range of 200 km for an aircraft with an RCS of 3m² with a LDSD detection range of 200 km for 16m² and a LDSD track range of 150 km for an aircraft with an RCS of 3m² with a rangefinding radar gun engagement range up to 10 km with a tracking scan range of 120° in azimuth and -60°/+70° in elevation with a full scan sweep in 0.2 seconds with LPI target engagement with over 100 frequency hops per second and an engagement range of 200 km vs 3m² with max tracking target velocity up to 6300 kph and stores tracking information for up to 6 non tracked targets with predictive flight paths for non tracked targets up to 13 seconds with LDSD ground clutter rejection of 80> dB with low chaff rejection with a MTBF of 100 to 200 hours)


(B model adds Zaslon-A radar with a 120° primary horizontal scan range and -60°/+70° vertical scan range enabling tracking of up to 14 targets and data linking of 4 missiles with an Rmax range of 300 km, in 15-24° STTR narrow beam mode detection range is 200 to 250 km vs RCS of 5m², 100 to 150 km vs RCS of 1m² and 80 to 100 km vs RCS of 0.1m², normal detection range of 210 km for an aircraft with an RCS of 16m² and a track range of 120 to 180 km for an aircraft with an RCS of 3-16m² with a LDSD detection range of 120 km for 16m² and a LDSD track range of 80 km for an aircraft with an RCS of 16m² with a rangefinding radar gun engagement range up to 10 km with a tracking scan range of 120° in azimuth and -60°/+70° in elevation with a full scan sweep in 0.2 seconds with max tracking target velocity up to 6300 kph and stores tracking information for up to 4 non tracked targets with predictive flight paths for non tracked targets up to 10 seconds with LDSD ground clutter rejection of 80> dB with low chaff rejection with a MTBF of 100 to 200 hours)


(31BM adds Zaslon-AM radar with a 120° primary horizontal scan range and -60°/+70° vertical scan range enabling tracking of up to 26 targets and data linking of 8 missiles with an Rmax range of 400 km, in 15-24° STTR narrow beam mode detection range is 300 to 350 km vs RCS of 5m², 150 to 200 km vs RCS of 0.1m² and 50 to 80 km vs RCS of 0.001m², normal detection range of 320 km for an aircraft with an RCS of 16m² and a track range of 200 km for an aircraft with an RCS of 5m² with a LDSD detection range of 200 km for 16m² and a LDSD track range of 150 km for an aircraft with an RCS of 5m² with a max ground attack detection range up to 400 km with a 140 km track range for tank sized targets with tracking of 10 ground targets and locking of up to 4 with SAR imaging up to 300 km, with base image resolutions of 1, 3 and 30 m at a spatial resolution size of 60, 150 and 300 km with radar imaging complete in 30 seconds with a rangefinding radar gun engagement range up to 10 km with a tracking scan range of 120° in azimuth and -60°/+70° in elevation with a full scan sweep in 0.2 seconds with LPI target engagement with over 100 frequency hops per second and an engagement range of 200 km vs 5m² with max tracking target velocity up to 6300 kph and stores tracking information for up to 10 non tracked targets with predictive flight paths for non tracked targets up to 12 seconds with LDSD ground clutter rejection of 80> dB with low chaff rejection with a MTBCF of 200 to 300 hours) 


Countermeasures: SPO-10 Sirena-3M 1st Generation solid state RWR with 4 targets tracked with 4× receivers enabling a self protection envelope of 360° in azimuth and ±90° in elevation with band coverage of 6-20 GHz. SSP-1 analogue fire countermeasure system. KM-1M ejection seat. SO-63/SRZO-2M 1st Generation solid state IFF interrogator / transponder linked to the Kremnij-2M2 analogue secure IFF system with aircraft ID,  and basic data encryption. CU32-SORC analogue ICAS. KKO-5LP solid state full ECLSS. 


(1975> and PD model adds, zero-zero ejection seat and SO-69/SRZO-1P 2nd Generation solid state IFF interrogator/transponder linked to the Parol digital IFF system with aircraft ID, digital data encryption reprogramming and cryptographic encoding)


(31 adds L-006M/SPO-15LM Beryoza-LM 2nd Generation digital RHAWS with 8 targets tracked with 6 preprogrammed threat identifiers and 5× receivers enabling a self protection envelope of 360° in azimuth and ±60° in elevation with band coverage of 4.4-10.3 GHz with a signal detectability range up to 225 km. SSP-2I digital fire countermeasure system. K-36DM Zero-Zero ejection seats. UV-3A countermeasure dispenser utilising 1st Generation IRCM and RFCM with 60 total rounds using the PPR-50 composite aluminium chaff that activates in 0.3 seconds and creates a false target RCS of greater than 60m² and using the PPI-50 thermite based flare with a minimum burn time of 3 seconds. SO-69/SRZO-1P 2nd Generation solid state IFF interrogator / transponder linked to the Parol digital IFF system with aircraft ID, digital data encryption reprogramming and cryptographic encoding. P-591 digital ICAS. KKO-15LP digital full ECLSS) 


(31M model added L-150/SPO-32 Pastel 3rd Generation fully digital RHAWS with 16 targets tracked and 128> preprogrammed threat identifiers with guidance of up to 6 ARMs with 2 fired simultaneous and 10× receivers enabling a self protection envelope of 360° in azimuth and ±60° in elevation with band coverage of 1.2-18 GHz with a signal detectability range up to 320 km. SO-72/SRZO-2P 2nd Generation digital IFF interrogator/transponder linked to the Parol-2D fully digital IFF system with aircraft ID, full digital data encryption, radio/inertial navigation locating, reprogramming and cryptographic encoding)


(BM model adds SO-96/SRZ-035M 3rd Generation fully digital IFF interrogator / transponder linked to the Parol-2D fully digital IFF system with aircraft ID, full digital data encryption, radio/inertial navigation locating, reprogramming and cryptographic encoding)


(From early 2020s onwards Parol-2D is replaced by Password-3 all digital IFF system with aircraft ID, low observability data sharing, satellite navigation locating, full digital data encryption, reprogramming and cryptographic encoding)


Electronic Warfare: N/A


(31M model adds BKO-16 self protection complex with L-001SP Smalta-SK 3rd Generation digital SPJ utilising radio direction finder with AoA and PRF determination, monopulse countermeasure, continuous wave countermeasure and pulse doppler countermeasure ECCM with track breaker, track breaking and blip enhancement ELINT with 8× receivers enabling an ECCM protection envelope of 360° in azimuth with a self protection jamming range of 200 km> with SPS-171M 3rd Generation digital active jamming system operating on 6-10 GHz with deception jamming, noise jamming, sweep jamming, pulse jamming, cross eye jamming, base jamming, spot jamming, wave jamming and power managed jamming ECM with 4× PESA pyramidal horn antenna ECM transmitters enabling an active jamming range of 200 km>)


(BM models add L-370K-31 Vitebsk-31 4th Generation fully digital SPJ utilising radio direction finder with AoA and PRF determination, simultaneous monopulse countermeasure, continuous wave countermeasure, pulse doppler countermeasure and LPIR countermeasure with doppler shifting, home on jam and anti burn though ECCM with track breaker, advanced decoy generation, blip enhancement and global navigation spoofing ELINT with frequency agile deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, spot jamming, wave jamming, power managed jamming and DRFM/ISRJ jamming ECM with 8× antennas enabling an ECCM protection envelope of 360° azimuth and a self protection jamming range of 300 km>)



Guns: N/A

(31 Models adds GSh-6-23 23×115mm rotary cannon slaved to radar with an effective firing range up to 1 km with a max fire rate up to 10,000 rpm)


Ordinance Capacity: 4× hardpoints with a max 2000 kg munition capacity.


(31 adds 8× hardpoints with a max munition capacity of 10,000 kg and up to 800 rounds for the gun) 


(31M model adds 10× hardpoints)


Common Air to Air Payloads for 25 

● 4× APU-40 racks with 2x R-40T and 2x R-40R

● 2× APU-40 racks with R-40R 2× APU-60-II dual racks with R-60


R-40R

3rd Generation Radar Missile 

PARG-12VV Inverse Monopulse J band Semi Active Seeker with a solid state inverse radiator cassegrain antenna array with an INS utilising a radio correction data link with back up inertial operting guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser proximity fuse with a high explosive blast warhead enabling a blast radius of 10-15 m²

~90 km max Range at 20 km+ altitude 

~70 km max Range at 10 km+ altitude 

~30 km max Range at sea level 

~15 km engagement range vs RCS of 16m² at sea level 

~50 km engagement range vs RCS of 16m² at 10 km+ altitude 

~70 km engagement range vs RCS of 16m² at 20 km+ altitude 

~6 km NEZ range vs RCS of 16m² at sea level 

~10 km NEZ range vs RCS of 16m² at 10 km> altitude

~30 km NEZ range vs RCS of 16m² at 20 km> altitude

~Mach 5 at 20 km+ altitude 

~Mach 4 at 10 km+ altitude 

~Mach 3 at sea level 

~Targeting Angles 20°

~Turn Rate 12 to 18 Deg/s

~Initial Acceleration of 300-500 m/s>

~Launch limiter 4g 

~Target limiter 5g 

~Overload Tolerance 24g 


R-40T

2nd Generation IR Missile 

TG-46 LN² Cooled solid state PIR channel Conical Scanning PbS Seeker

~50 km max Range at altitude 

~20 km max Range at sea level 

~30 km engagement range 

~Side aspect lock range 2 km

~Rear aspect lock range 20 km

~Mach 4 at 10 km+ altitude 

~Mach 3 at sea level 

~Rectile Speed: 70 Hz

~Gimbal limit: 40°

~Angular Tracking: 12 deg/s 

~Turn Rate 12 to 18 Deg/s

~Initial Acceleration of 300-500 m/s>

~Flare Resistance 0.2

~Launch limiter 4g 

~Target limiter 5g 

~Overload Tolerance 24g 


R-60

2nd Generation IR Missile 

OGS-60TI Komar analogue electronic MWIR channel Conical Scanning PbSe Seeker

~12 km max Range 

~12 km max Range at sea level 

~8 km engagement range 

~Side aspect lock range 1 km

~Rear aspect lock range 5 km

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Rectile Speed: 100 Hz

~Flare Resistance 0.2

~Gimbal limit: 12°

~Angular Tracking: 35 deg/s 

~Turn Rate 60 to 90 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 8g 

~Target limiter 12g 

~Overload Tolerance 42g 


25PD model adds 


Common Air to Air Payloads 

● 4× APU-40 racks with 2x R-40TD and 2x R-40RD 

● 2× APU-40 racks with R-40RD 2× APU-60-II dual racks with R-60M


R-40RD

3rd Generation Radar Missile 

PARG-12-VVD Inverse Monopulse J band Semi Active Seeker with a inverse radiator cassegrain antenna array with an INS utilising a radio correction data link with back up inertial operting guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser proximity fuse with a high explosive blast warhead enabling a blast radius of 10-15 m²

~100 km max Range at 20 km+ altitude 

~80 km max Range at 10 km+ altitude 

~50 km max Range at sea level 

~30 km engagement range vs RCS of 16m² at sea level 

~60 km engagement range vs RCS of 16m² at 10 km+ altitude 

~80 km engagement range vs RCS of 16m² at 20 km+ altitude 

~10 km NEZ range vs RCS of 16m² at sea level 

~20 km NEZ range vs RCS of 16m² at 10 km> altitude

~30 km NEZ range vs RCS of 16m² at 20 km> altitude

~Mach 5 at 20 km+ altitude 

~Mach 4 at 10 km+ altitude 

~Mach 3 at sea level 

~Targeting Angles 20°

~Turn Rate 12 to 18 Deg/s

~Initial Acceleration of 300-500 m/s>

~Launch limiter 4g 

~Target limiter 5g 

~Overload Tolerance 24g 


R-40TD

2nd Generation IR Missile 

TG-46 LN² Cooled solid state PIR channel Conical Scanning PbS Seeker

~50 km max Range at altitude 

~30 km max Range at sea level 

~40 km engagement range 

~Side aspect lock range 4 km

~Rear aspect lock range 20 km

~Mach 4.5 at 10 km+ altitude 

~Mach 4 at 5 km+ altitude 

~Mach 3 at sea level 

~Rectile Speed: 100 Hz

~Flare rejection 0.2

~Gimbal limit: 40°

~Angular Tracking: 12 deg/s 

~Turn Rate 12 to 18 Deg/s

~Initial Acceleration of 300-500 m/s>

~Launch limiter 4g 

~Target limiter 5g 

~Overload Tolerance 24g 



R-60M

3rd Generation IR Missile 

OGS-75 Komar-M thermoelectric Cooled digital MWIR channel Conical Scanning PbSe Seeker

~12 km max Range at altitude 

~12 km max Range at sea level 

~8 km engagement range 

~All aspect lock range 2 km

~Rear aspect lock range 8 km

~Mach 3 at high altitude 

~Mach 2 at sea level 

~Rectile Speed: 120 Hz

~Flare rejection 0.4

~Gimbal limit: 17°

~Angular Tracking: 35 deg/s 

~Turn Rate 60 to 90 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 8g 

~Target limiter 12g 

~Overload Tolerance 42g 


31 model adds 


Common Air to Air Payloads 

● 4× AKU-33 racks with R-33 2× APU-40 racks with R-40TD1 2× APU-73 racks with R-73 

● 4× AKU-33 racks with R-33 4× APU-40 racks with R-40TD1


R-40TD1

4th Generation IR Missile 

Geofizika-35T1 LN² Cooled digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~70 km max Range at altitude 

~40 km max Range at sea level 

~50 km engagement range 

~All aspect lock range 20 km

~Rear aspect lock range 30 km

~Rectile Speed: 125 Hz

~Gimbal limit: 60°

~Angular Tracking: 20 deg/s 

~Turn Rate 12 to 18 Deg/s

~Initial Acceleration of 300-500 m/s>

~Launch limiter 4g 

~Target limiter 5g 

~Overload Tolerance 24g 

~Flare Resistance 0.6

~Mach 4.5 at 10 km+ altitude 

~Mach 4 at 5 km+ altitude 

~Mach 3 at sea level 


R-73

4th Generation IR Missile 

Mayak-80 LN² Cooled digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~30 km max Range at altitude 

~20 km max Range at sea level 

~20 km engagement range 

~All aspect lock range 4 km

~Rear aspect lock range 10 km 

~Mach 3 at high altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.6

~Gimbal limit: 45°

~Angular Tracking: 60 deg/s 

~Turn Rate 90 to 120 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 60g 


R-33

3+ Generation Radar Missile

MFBU-410 conopulse X band Semi Active Seeker with a digital parabolic reflector cassegrain antenna array with an INS utilising a radio correction data link and back up semi active channel engaged at terminal phase with back up inertial operting guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser proximity fuse with a high explosive blast warhead enabling a blast radius of 10-15 m²

~230 km max Range at 10 km+ altitude 

~150 km max Range at sea level 

~120 km engagement range vs RCS of 5m² at sea level 

~180 km engagement range vs RCS of 5m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 5m² at sea level 

~50 km NEZ range vs RCS of 5m² at 10 km> altitude

~70 km NEZ range vs RCS of 5m² at 20 km> altitude

~Mach 4 max target velocity 

~Mach 5 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 30°

~Turn Rate 10 to 17 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 8g 

~Target limiter 6g 

~Overload Tolerance 32g


GSh-6-23

AM-23 23×115mm SAPHEI


M and B model adds 


Common Air to Air Payloads 

● 6× AKU-33 racks with R-33S 2× APU-40 racks with R-40TD1 2× APU-73 racks with R-74

● 6× AKU-33 racks with R-33S 4× APU-40 racks with R-40TD1

● 6× AKU-33 racks with R-37 4× APU-40 racks with R-40TD1

● 6× AKU-33 racks with R-37 2× APU-40 racks with R-40TD1 2× APU-73 racks with R-74


R-33S

3+ Generation Radar Missile

MFBU-410S conopulse X band Semi Active Seeker with a digital parabolic cassegrain antenna array with an INS utilising a radio correction data link and back up semi active channel engaged at terminal phase with back up inertial operting guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser proximity fuse with a high explosive blast warhead enabling a blast radius of 10-15 m²

~230 km max Range at 10 km+ altitude 

~200 km max Range at sea level 

~160 km engagement range vs RCS of 5m² at sea level 

~200 km engagement range vs RCS of 5m² at 10 km+ altitude

~20 km NEZ range vs RCS of 5m² at sea level 

~70 km NEZ range vs RCS of 5m² at 10 km> altitude

~90 km NEZ range vs RCS of 5m² at 20 km> altitude

~Mach 4 max target velocity 

~Mach 5 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 30°

~Turn Rate 10 to 17 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 8g 

~Target limiter 6g 

~Overload Tolerance 32g


R-37

4th Generation Radar Missile 

9P-1388 conopulse X band Active Seeker with a digital parabolic cassegrain antenna array with an INS utilising a radio correction data link with back up inertial operting guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a radio proximity fuse and back up impact detonation with with a high explosive blast warhead enabling a blast radius of 10-15 m²

~300 km max Range at 10 km+ altitude 

~100 km max Range at sea level 

~70 km engagement range vs RCS of 5m² at sea level 

~200 km engagement range vs RCS of 5m² at 10 km+ altitude 

~50 km NEZ range vs RCS of 5m² at sea level 

~70 km NEZ range vs RCS of 5m² at 5 km> altitude

~90 km NEZ range vs RCS of 5m² at 10 km> altitude

~20 km ARH lock range vs RCS of 1m²

~40 km ARH lock range vs RCS of 5m²

~50 km ARH lock range vs RCS of 10m²

~8g launch limiter

~8g target limiter 

~Targeting Angles 45°

~Turn Rate 10 to 30 Deg/s

~Initial Acceleration of 300-500 m/s>

~40g overload tolerance 

~Mach 5 max target velocity 

~Mach 5 top speed above 5 km altitude 

~Mach 3 top speed at sea level



31BM prototype adds 

R-77-1A

4th Generation Radar Missile 

9B-1248 Inverse Monopulse X band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a bi-directional radio correction data link with back up inertial operting guidance, home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser and Z23nA radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~150 km max Range at 10 km+ altitude 

~120 km max Range at 5 km+ altitude 

~90 km max Range at sea level 

~50 km engagement range vs RCS of 5m² at sea level 

~90 km engagement range vs RCS of 5m² at 5 km+ altitude 

~120 km engagement range vs RCS of 5m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 5m² at sea level 

~30 km NEZ range vs RCS of 5m² at 5 km> altitude

~40 km NEZ range vs RCS of 5m² at 10 km> altitude

~6 km ARH lock range vs RCS of 1m²

~18 km ARH lock range vs RCS of 5m²

~24 km ARH lock range vs RCS of 10m²

~0.1 m² minimum target RCS for ARH lock 

~Mach 5 max target velocity 

~Mach 4 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~Launch limiter 9g 

~Target limiter 12g 

~Overload Tolerance 60g



31BM adds 


Common Air to Air Payloads 

● 4× AKU-410-1 with R-37M 4× AKU-170 with R-77-1 

● 4× AKU-410-1 with R-37M 2× AKU-170 with R-77-1 2× APU-73 racks with R-74M 


R-37M

4+ Generation Radar Missile 

9B-1103M-350 Inverse Monopulse Ku/X band Active Seeker with an fully digital slotted planar antenna array with an GNSS/INS and two way data link with back up inertial operting guidance, home on jam, dual band seeker and polarisation filtering ECCM utilising a solid fuel dual pulse rocket motor with a kolibri radio proximity fuse with back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-20 m²

~400 km max range at 10 km+ altitude 

~300 km max Range at 5 km+ altitude 

~150 km max Range at sea level 

~120 km engagement range vs RCS of 3m² at sea level 

~200 km engagement range vs RCS of 3m² at 5 km+ altitude 

~300 km engagement range vs RCS of 3m² at 10 km+ altitude 

~70 km NEZ range vs RCS of 3m² at sea level 

~90 km NEZ range vs RCS of 3m² at 5 km> altitude

~120 km NEZ range vs RCS of 3m² at 10 km> altitude

~20 km ARH lock range vs RCS of 1m²

~40 km ARH lock range vs RCS of 3m²

~70 km ARH lock range vs RCS of 10m²

~0.005 m² minimum target RCS for ARH lock 

~Targeting Angles 45°

~Turn Rate 10 to 60 Deg/s

~Initial Acceleration of 600-900 m/s>

~8g launch limiter

~8g target limiter 

~40g overload tolerance 

~Mach 6 max target velocity 

~Mach 6 top speed above 5 km altitude 

~Mach 4 top speed at sea level


R-77-1C

4+ Generation Radar Missile 

9B-1103M-200PA Inverse Monopulse Ku band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a bi-directional radio correction data link with back up inertial operting guidance, home on jam, multimode guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a laser and Z23nA radio proximity fuse and back up impact detonation with a high explosive blast warhead enabling a blast radius of 10-15 m²

~200 km max Range at 10 km+ altitude 

~150 km max Range at 5 km+ altitude 

~80 km max Range at sea level 

~50 km engagement range vs RCS of 3m² at sea level 

~100 km engagement range vs RCS of 3m² at 5 km+ altitude 

~120 km engagement range vs RCS of 3m² at 10 km+ altitude 

~20 km NEZ range vs RCS of 3m² at sea level 

~40 km NEZ range vs RCS of 3m² at 5 km> altitude

~60 km NEZ range vs RCS of 3m² at 10 km> altitude

~10 km ARH lock range vs RCS of 1m²

~20 km ARH lock range vs RCS of 3m²

~30 km ARH lock range vs RCS of 10m²

~0.05 m² minimum target RCS for ARH lock 

~Mach 5 max target velocity 

~Mach 4 top speed above 5 km altitude 

~Mach 2 top speed at sea level

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~Launch limiter 9g 

~Target limiter 12g 

~Overload Tolerance 60g


R-74M

4+ Generation IR Missile 

Impuls-90 LN² Cooled NIR & UV channel fully digital pseudo-imaging HgCdTe Seeker with dual band, gatewidth and seeker shut off IRCCM

~50 km max Range at altitude 

~30 km max Range at sea level 

~40 km engagement range 

~All aspect lock range 10 km

~Rear aspect lock range 10 km 

~Mach 3 at 5 km> altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.8

~Gimbal limit: 75°

~Angular Tracking: 60 deg/s 

~Turn Rate 120 to 180 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 80g 


MiG-25 (prototype) 


MiG-25P


MiG-25PD



MiG-31A


MiG-31B

MiG-31M


MiG-31BM (Prototype) 

MiG-31BM (Production) 





MiG-23 Flogger Family 


MiG-23S 

Designed: 1964

Prototype: 1967

Completed: 1968

Production: 1969

Service: 1970

Generation: 3rd

Aircraft Role: Interceptor/Fighter

Number Made: 2000+

Combat Rank: S


MiG-23M 

Designed: 1969

Prototype: 1972

Completed: 1972

Production: 1974

Service: 1974

Generation: 3+

Aircraft Role: Interceptor/Fighter

Number Made: 3000+

Combat Rank: C


MiG-23ML

Designed: 1972

Prototype: 1975

Completed: 1975

Production: 1976

Service: 1977

Generation: 3+

Aircraft Role: Interceptor/Fighter

Number Made: 1000+

Combat Rank: A


MiG-23MLA

Designed: 1976

Prototype: 1977

Completed: 1977

Production: 1978

Service: 1979

Generation: 3+

Aircraft Role: Interceptor/Fighter

Number Made: 600+

Combat Rank: A


MiG-23P

Designed: 1975

Prototype: 1976

Completed: 1978

Production: 1979

Service: 1980

Generation: 3+

Aircraft Role: Interceptor/Fighter

Number Made: 500+

Combat Rank: D


MiG-23MLD

Designed: 1977

Prototype: 1981

Completed: 1982

Production: 1983

Service: 1985

Generation: 4th

Aircraft Role: Interceptor/Fighter

Number Made: 500+

Combat Rank: B


MiG-23-98

Designed: 1991

Prototype: 1994

Generation: 4th

Aircraft Role: Interceptor/Fighter

Number Made: 4

Combat Rank: D


Engine and Airframe: All metal construction with an RCS minimum of 8m². Crew of 1. Length 16.7 m. Height 4.8 m. Wingspan 7-14 m. Wing area 34-37 m². Frame weight 12,0840 kg. Takeoff weight 17,800 kg. Max Fuel 2,800 kg. Tumansky R-29-300 axial flow turbojet with an analogue electronic engine control with 82 kN of thrust and 123 kN in afterburner. 


Speed and Endurance: Top speed of mach 2.2 to 2.5 at 15 km+, mach 2.1 to 2.4 at 10 km+, mach 1.8 to 2 to at 5 km+ and mach 1 to 1.3 at sea level. Service Ceiling of 18 to 20 km. Combat range of 1400-1900 km. Acceleration 10-16 seconds to mach 1 at sea level. Stall speed 270-310 kph. 


Manuvarabilities: Thrust to weight ratio of 0.7 at full air to air payload and 0.9 at half fuel/loadout. Roll rate of 140 deg/s at high speed and 170 deg/s at low speed. Climb rate of 200-220 m/s. Angle of Attack at 22° at mach 2>, 24° at mach 1> and 25° at mach <1. 20 to 120 kph/s speed bleed at high g instantaneous maneuvers and 30 to 80 kph/s speed bleed at high g sustained maneuvers. Sustained G tolerance of 7g and a max Overload Tolerance of 9g with wing break at 12g. Wing loading of 370-390 kg/m². 2× LERXs with pitch of ±20°.


(ML, MLA, P and MLD model adds Thrust to weight ratio of 0.8 at full air to air payload and 1 at half fuel/loadout. Thrust to weight ratio of 0.7 at full air to air payload and 1.1 at half fuel/loadout. Roll rate of 140 deg/s at high speed and 170 deg/s at low speed. Climb rate of 200-220 m/s. Angle of Attack at 28° at mach 2>, 30° at mach 1> and 33° at mach <1. 10 to 70 kph/s speed bleed at high g instantaneous maneuvers and 20 to 50 kph/s speed bleed at high g sustained maneuvers. Overload tolerance of 10g and sustained at 8g)


Aircraft Turn Rates 


Sustained turn rates 


Mach ~1.5 Speeds 

● 1 deg/s at 5 km altitude 

● 1-4 deg/s at sea level 


Mach ~1 Speeds 

● 6-7 deg/s at 10 km altitude 

● 7-9 deg/s at 5 km altitude 

● 9-12 deg/s at sea level 


Mach ~0.5 Speeds 

● 9-11 deg/s at 10 km altitude 

● 11-14 deg/s at 5 km altitude 

● 13-17 deg/s at sea level 


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 2-3 deg/s at 10 km altitude 

● 4-6 deg/s at 5 km altitude 

● 8-11 deg/s at sea level  


Mach ~1 Speeds 

● 9-11 deg/s at 10 km altitude 

● 10-13 deg/s at 5 km altitude 

● 15-19 deg/s at sea level  


Mach ~0.5 Speeds 

● 10-13 deg/s at 10 km altitude 

● 12-16 deg/s at 5 km altitude 

● 17-22 deg/s at sea level  


ML model onwards add 


Sustained turn rates 


Mach ~1.5 Speeds 

● 1-2 deg/s at 5 km altitude 

● 2-5 deg/s at sea level


Mach ~1 Speeds 

● 6-7 deg/s at 10 km altitude 

● 8-10 deg/s at 5 km altitude 

● 10-13 deg/s at sea level 


Mach ~0.5 Speeds 

● 10-12 deg/s at 10 km altitude 

● 12-15 deg/s at 5 km altitude 

● 15-19 deg/s at sea level 


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 3-4 deg/s at 10 km altitude 

● 5-7 deg/s at 5 km altitude 

● 9-11 deg/s at sea level  


Mach ~1 Speeds 

● 8-10 deg/s at 10 km altitude 

● 11-14 deg/s at 5 km altitude 

● 16-20 deg/s at sea level  


Mach ~0.5 Speeds 

● 13-16 deg/s at 10 km altitude 

● 15-19 deg/s at 5 km altitude 

● 20-25 deg/s at sea level  


Airframe RCS

RCS Minimum: 8m²

RCS Median: 9m²

RCS Average: 10-13m²


Targeting: Sapfir-21MA radar with a horizontal scan range of 60° and ±10° vertical scan range enabling an Rmax range up to 30 km, with a detection range of 25 km for 16m² and a track range of 17 km for an aircraft with an RCS of 16m² with a rangefinding radar gun engagement range up to 2 km with a tracking scan range of 30° in azimuth and ±6° in elevation with a scan sweep in 3 to 5 seconds with max tracking target velocity at over 2500 kph with very low chaff rejection with a MTBF of 10 to 30 hours.


(M model adds Sapfir-23D radar with a horizontal scan range of 104° and -38°/+43° vertical scan range enabling an Rmax range up to 70 km, with a detection range of 60 km for 16m² and a track range of 30 km for an aircraft with an RCS of 16m² with a LDSD detection range of 20 km for 16m² and a LDSD track range of 10 km for an aircraft with an RCS of 16m² with a rangefinding radar gun engagement range up to 9 km with a tracking scan range of 60° in azimuth and -8.5°/+12° in elevation with a scan sweep in 3.5 seconds with max tracking target velocity at over 2500 kph with LDSD ground clutter rejection of 20> dB with very low chaff rejection with a MTBF of 10 to 30 hours. TP-23 IRST with single target tracking with an angular resolution of 1° and max tracking rate of 6 deg/s enabling a max tracking rate of 8 deg/s enabling a max range up to 50 km with a 20 to 40 km detection range 10 to 15 km rear track range with 6 km front track range for fighter sized targets with a horizontal FOV up to 60° and a vertical FOV of ±7°)


(1974+ M models add Sapfir-23D-III radar with a horizontal scan range of 104° and -38°/+43° vertical scan range enabling an Rmax range up to 70 km, with a look up detection range of 65 km for 16m² and a track range of 42 km for an aircraft with an RCS of 16m² with a LDSD detection range of 22 km for 16m² and a LDSD track range of 12 km for an aircraft with an RCS of 16m² with a rangefinding radar gun engagement range up to 9 km with a tracking scan range of 60° in azimuth and -8.5°/+12° in elevation with a scan sweep in 3.5 seconds with max tracking target velocity at over 2500 kph with LDSD ground clutter rejection of 20> dB with very low chaff rejection with a MTBF of 10 to 30 hours)


(ML models add Sapfir-23ML radar with a horizontal scan range of 112° and -44°/+56° vertical scan range with an Rmax range up to 90 km, with a detection range of 72 km for 16m² and a track range of 52 km for an aircraft with an RCS of 16m² with a LDSD detection range of 24 km for 16m² and a LDSD track range of 14 km for an aircraft with an RCS of 16m² with a rangefinding radar gun engagement range up to 9 km with a tracking scan range of 60° in azimuth and -7°/+7° in elevation with a scan sweep in 3.5 seconds with max tracking target velocity at over 2500 kph with LDSD ground clutter rejection of 30> dB with low chaff rejection with a MTBF of 10 to 40 hours. TP-23ML with single target tracking with an angular resolution of 1° and max tracking rate of 8 deg/s enabling a max detection range up to 55 km with a 20 to 45 km detection range 12 to 17 km rear track range with 6 km front track range for fighter sized targets with a horizontal FOV up to 60° and a vertical FOV of -7°/+7°)


(P model adds Sapfir-23P radar with a horizontal scan range of 112° and -44°/+56° vertical scan range with with an Rmax range up to 90 km, with a detection range of 75 km for 16m² and a track range of 52 km for an aircraft with an RCS of 16m² with a LDSD detection range of 40 km for 16m² and a LDSD track range of 20 km for an aircraft with an RCS of 16m² with a rangefinding radar gun engagement range up to 9 km with a tracking scan range of 60° in azimuth and -6°/+6° in elevation with a scan sweep in 3.5 seconds with max tracking target velocity at over 2500 kph with LDSD ground clutter rejection of 40> dB with low chaff rejection with a MTBCF of 10 to 40 hours)


(MLD model adds Sapfir-23MLA-II radar with a horizontal scan range of 112° and -44°/+56° vertical scan range enabling tracking of up to 2 targets with an Rmax range up to 90 km, with a detection range of 75 km for 16m² and a track range of 52 km for an aircraft with an RCS of 16m² with a LDSD detection range of 42 km for 16m² and a LDSD track range of 23 km for an aircraft with an RCS of 16m² with a rangefinding radar gun engagement range up to 9 km with a tracking scan range of 60° in azimuth and -6°/+6° in elevation with a scan sweep in 3.5 seconds with max tracking target velocity at over 2500 kph with LDSD ground clutter rejection of 40> dB with low chaff rejection with a MTBF of 10 to 40 hours. TP-26 IRST with single target tracking with an angular resolution of 0.5° and max tracking rate of 8 deg/s enabling a max detection range up to 70 km with a 30 to 60 km detection range 15 to 20 km rear track range with 6 km front track range for fighter sized targets with a horizontal FOV up to 60° and a vertical FOV of -7°/+7°)


(98 model adds Moskit-23 pulse doppler radar with 120° horizontal and -10°/+30° vertical scan range enabling tracking of up to 10 targets and data linking of 2 missiles with an Rmax range up to 120 km, detection range of 90 km for 16m² and a 60 km track range for an aircraft with an RCS of 3m² with a horizontal SNP scan range of 40° and a horizontal SNP scan time of 2 seconds with max tracking target velocity at over 3000 kph and stores tracking information for up to 2 non tracked target with predictive flight paths for non tracked targets up to 10 seconds with LDSD ground clutter rejection of 70> dB. Shchel-3UM HMD with a 120° horizontal FOV and -30°/+30° vertical FOV utilising automatic cueing for targeting with head tracking software)


Targeting Pods for 98 model 

Kopyo-25 2nd Generation Targeting Pod with a 3rd Generation fully digital PESA GAR utilising a slotted planar array with max detection range up to 40 km with a 20 km track range for tank sized targets with tracking of up to 10 targets and locking of up to 2. 


Navigation & Flight Control: Polyot-11-23 analogue navigation suite with an NVU-23 analogue electronic navigation computer using a SKV-2N-2 mechanical gimballed gyrostabilized accelerometer INS. ARK-14 analogue ADF. RSBN-6S Romb-1K solid state radio navigation system with VOR with a position accuracy of 300-700m and angular accuracy of ±1°. RV-4 analogue radar altimeter. SAU-23A 3× axis electromechanical autopilot with BU-190-270 hydraulic AFCS with a SVS-23 nuvistor ADC. ZSh-3 Flight Helmet. 


Communication & C2: Klyon analogue electronic communication complex with the RSIU-5V VHF analogue electronic radio with 2 way communication, FM and AM receiving and built in IAD with voice formats with 20 pre set channels with an operating communication range of 200 km. Vozdukh-1M analogue electronic GCI complex with the ARL-SM Lazour-M analogue electronic navigation and command Data Link connected with the SAU-23A electromechanical autopilot, ARK-10 analogue ADF, SO-57M interrogator and SRZO-2M analogue electronic IFF transponder linked to the Voyska PVO Strany URAGAN air defence network with fully automated ground controlled interception, data encryption and IFF integration utilising ground and air based radar and computer generated data exchange with pre recorded sound and text formats used, with data transfer speeds of 54 bit/s every 4 to 5 seconds enabling a LOS data transmission range up to 350 km with data exchange between 3 aircraft


Fire Control: Sokol-23 electromechanical FCS with angle of slide, angle of attack, air speed, altitude and aircraft position computed with analogue systems with RLPK-23 radar targeting. RP-22SMA Sapfir-21M 2nd Generation mechanically steered J band analogue electronic monopulse radar system with a C band beacon interrogator with a inverse radiator cassegrain antenna array with analogue signal processing, P, K, E and C scope radar image displayed with CW illumination for SARH guidance and IFF integration with multi mode operating function and raster, conical, and spiral scan scanning modes utilising SRC, STTR and RFR ACM air to air radar modes with gain modulation and polarization filtering ECCM with LPRF power output on average being 100-200 W with a 40 kW max output with a 520 mm antenna diameter. ITO-1 3rd Generation Radar display with a CRT screen utilising a K/E oscilloscope for target engagement and a P/C oscilloscope for target search. ASP-PFD 2nd Generation HUD with an analogue electronic CRT collimator reflector utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with gun, bomb and rocket CCRP and CCIP 


(M model adds Sokol-23M electromechanical FCS with angle of slide, angle of attack, air speed, altitude and aircraft position computed with analogue systems with RLPK-23M radar targeting and STP infrared tracking targeting. RP-23 Sapfir-23D 2+ Generation J band mechanically steered analogue electronic long chord twist cassegrain antenna arrays with a C band beacon interrogator with analogue signal processing, P, K, E and C scope radar image displayed with MTI based LDSD, CW illumination for SARH guidance and IFF integration with multi mode operating function and raster, conical, and spiral scan scanning modes utilising SRC/LDSD, STTR and IRST and RFR based ACM air to air radar modes with gain modulation and polarization filtering ECCM with LPRF power output on average being 200-270 W with a 60 kW max output with a 800 mm antenna diameter. ASP-23D 3rd Generation HUD with a solid state CRT collimator reflector utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with gun, bomb and rocket CCRP and CCIP with gun EEGS with an integrated 3rd Generation Radar display with a holographic screen utilising a K/E oscilloscope for target engagement and a P/C oscilloscope for target search. TP-23 1st Generation IRST utilising a LN² cooled conical scanning PbS detector. AVM-23 electromechanical ballistic computer enabling gun and missile coursing. Evkalipt solid state communication system with the R-855/R-832 VHF/UHF and R-802 HF solid state radios with 2 way communication, FM and AM receiving, built in IAD and secure voice encryption with voice formats utilised operating on 120 pre set channels with an operating communication range of 300 km)


(1974+ M models add RP-23M Sapfir-23D-III)


(Export MF and MS models retained RP-22SMA Sapfir-21S and Sokol-23 FCS)


(ML models add Sokol-23ML digitised FCS with angle of slide, angle of attack, air speed, altitude and aircraft position computed with analogue systems with RLPK-23 radar targeting and STP infrared tracking targeting. PrNK-23ML digital/analogue navigation system with a SAU-23AM 3× axis electromechanical autopilot and a BU-23M hydromechanical AFCS utilising an TsSVM-23 4x bit ADC with a 10-70k SLOC-OS with electronic flight control. with a KN-23 digital navigation system. RV-4M radar altimeter, N003 Sapfir-23ML 2+ Generation J band mechanically steered solid state long chord twist cassegrain antenna arrays with a C band beacon interrogator with analogue signal processing, BIST system and P, K, E and C scope radar image displayed with MTI based LDSD, CW illumination for SARH guidance and IFF integration with multi mode operating function and raster, conical, and spiral scan scanning modes utilising SRC/LDSD, STTR and IRST and RFR based ACM air to air radar modes with gain modulation and polarization filtering ECCM with LPRF power output on average being 200-270 W with a 70 kW max output with a 800 mm antenna diameter.  ASP-23DTsM 3rd Generation HUD with a solid state CRT collimator reflector utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with gun, bomb and rocket CCRP and CCIP with gun EEGS with an integrated 3rd Generation Radar display with a holographic screen utilising a K/E oscilloscope for target engagement and a P/C oscilloscope for target search. TP-23ML 1st Generation IRST utilising a LN² cooled conical scanning PbS detector and option for ZSh-3 Helmet with Schel-3 Gen 0 HMD)


(Export ML models used N003 Sapfir-23E with massively reduced LDSD and no ECCM)


(MLA model adds N004 Sapfir-23MLA 2+ Generation J band mechanically steered solid state long chord twist cassegrain antenna arrays with a C band beacon interrogator with analogue signal processing, BIST system and P, K, E and C scope radar image displayed with MTI based LDSD, CW illumination for SARH guidance and IFF integration with multi mode operating function and raster, conical, and spiral scan scanning modes utilising SRC/LDSD, STTR and IRST and RFR based ACM air to air radar modes with gain modulation and polarization filtering ECCM with LPRF power output on average being 200-270 W with a 70 kW max output with a 800 mm antenna diameter)


(Export MLA models used N003 Sapfir-23MLAE with reduced LDSD and reduced ECCM)


(P model adds Sokol-23P computerised FCS with angle of slide, angle of attack, air speed, altitude and aircraft position computed digitally with RLPK-23 radar targeting and STP infrared tracking targeting. N006 Sapfir-23P 2+ Generation J band mechanically steered solid state long chord twist cassegrain antenna arrays with a C band beacon interrogator with analogue signal processing, BIST system and P, K, E and C scope radar image displayed with MTI based LDSD, CW illumination for SARH guidance and IFF integration with multi mode operating function and raster, conical, and spiral scan scanning modes utilising SRC/LDSD, STTR and IRST and RFR based ACM air to air radar modes with gain modulation and polarization filtering ECCM with LPRF power output on average being 200-270 W with a 70 kW max output with a 800 mm antenna diameter. PrNK-23P digital nav/attack suite with a SAU-23P 3× axis computerised autopilot and a SUU-23P digital electro hydraulic AFCS utilising a Ts-040 4x bit digital ADC, ASP-23DTsM-P 3rd Generation HUD with a solid state CRT collimator reflector utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayedwith gun EEGS with an integrated 3rd Generation Radar display with a holographic screen utilising a K/E oscilloscope for target engagement and a P/C oscilloscope for target search, Rubezh digital GCI complex with the Biryusa digital navigation data link and BAN-75, SVPK, SPK-75 and SPK-68 digital command data links connected to the SAU-155P1 autopilot, ARK-19 solid state ADF, SO-69 solid state IFF interrogator and SRZO-2P solid state IFF transponder linked to the PVO NDCC air defence network with fully automated ground controlled interception, weapons management, IFF integration, digital data encryption and navigation data utilising ground based computer and radar generated data exchange with pre recorded voice and text formats used with data transfer speeds of 45 bit/s, 80 bit/s and 96 bit/s every 5 to 10 seconds operating on 2 MHz to 400 MHz with up to 20,000 frequency hops per second on 20+ frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1000 km with data exchange between up to 36 aircraft)


(MLD model adds Sokol-23MLD computerised FCS with angle of slide, angle of attack, air speed, altitude and aircraft position computed digitally with RLPK-23 radar targeting and STP infrared tracking targeting with an Orbita-10-23 digital FCC utilising K155 4x bit CPUs performing 90-125k IPS and 5-10m FLOPS. PrNK-23MLD computerised nav/attack suite with a SAU-23-18 3× axis computerised autopilot and a SUU-18 solid state electro hydraulic AFCS utilising a Ts-040-2 8x bit digital ADC, N008 Sapfir-23MLA-II 2++ Generation J band mechanically steered solid state long chord twist cassegrain antenna array with a C band beacon interrogator with analogue to digital signal processing, BIST system and P, K, E and C scope radar image displayed with MTI based LDSD, CW illumination for SARH guidance and IFF integration with multi mode operating function and raster, conical, and spiral scan scanning modes utilising SRC/LDSD, MTTR, STTR and IRST and RFR based ACM air to air radar modes with gain modulation and polarization filtering ECCM with LPRF power output on average being 200-270 W with a 70 kW max output with a 800 mm antenna diameter. and ASP-17ML 3rd Generation HUD with a solid state CRT collimator reflector utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with gun, bomb and rocket CCRP and CCIP with gun EEGS with an integrated 3rd Generation Radar display with a holographic screen utilising a K/E oscilloscope for target engagement and a P/C oscilloscope for target search. TP-26 1st Generation IRST utilising a LN² cooled conical scanning InSb detector. TsVB-23B digital ballistic computer utilising a 580VM80 8x bit CPU enabling gun and missile coursing with gun and bomb CCIP and CCRP)


(Export MLD models used N003 Sapfir-23MLAE-II MTI radar with full LDSD and ECCM but no SNP multi track and tracking beyond limits removed and used 60° scan)


(98 model adds Moskit computerised FCS utilising Ts-101 digital FCC utilising K1801 16x bit CPUs performing 300-400k IPS and 150-200m FLOPS. Moskit-23 3rd Generation digital X band pulse doppler radar with a mechanically steered slotted planar array with power output on average being 1-2 kW with a 5 kW max output with a 700 mm antenna. TsVB-98 digital ballistic computer utilising a KM1810VM88 16x bit CPU enabling automatic digital target lead with gun, rocket and bomb CCRP and CCIP with a max bomb and rocket accuracy of <10-20m CEP at a range up to 2000m and altitudes up to 3000m and <100-300m CEP at a range up to 10,000m and altitude up to 10,000m. R-800 and R-862 VHF/UHF and R-864 HF Digital radios. ZSh-7 Helmet with Shchel-3UM 1st Generation HMD. ILS-31 4th Generation digital HUD with an integrated digital bombing complex with gun, bomb and rocket CCRP and CCIP with full gun EEGS. 4th Generation Radar display with an SVD system utilising a CRT display with a polychrome raster image)


Countermeasures: SPO-10 Sirena-3M 1st Generation solid state RWR with 4 targets tracked with 4× receivers enabling a self protection envelope of 360° in azimuth and ±90° in elevation with band coverage of 6-20 GHz. SSP-1 analogue fire countermeasure system. KM-1M ejection seat. SO-57M/SRZO-2M 1st Generation analogue electronic IFF interrogator / transponder linked to the Kremnij-2M2 analogue secure IFF system with aircraft ID and basic analogue data encryption. CU32-SORC analogue ICAS. KKO-5LP solid state full ECLSS. 


(M model onwards had options for ASO-2I countermeasure dispenser utilising 1st Generation IRCM and RFCM with 68 total rounds using the PPR-26-13 composite aluminium chaff that activates in 0.3 seconds and creates a false target RCS of greater than 30m² and using the PPI-26 thermite based flare with a minimum burn time of 3 seconds)


(ML model onwards had SO-69/SRZO-1P 2nd Generation solid state IFF interrogator / transponder linked to the Parol fully digital IFF system with aircraft ID, digital data encryption reprogramming and cryptographic encoding. had option for BVP-30-26 1st Generation IRCM and 2nd Generation RFCM with 60 chaff and flares)


(MLD model adds L-006M/SPO-15LM Beryoza-LM 2nd Generation digital RHAWS with 8 targets tracked with 6 preprogrammed threat identifiers with 5× receivers enabling a self protection envelope of 360° in azimuth and ±60° in elevation with band coverage of 4.4-10.3 GHz with a signal detectability range up to 225 km. BVP-50-60 countermeasure dispenser utilising 1st Generation IRCM and RFCM with 56 total rounds using the PPR-26-13 composite aluminium chaff that activates in 0.3 seconds and creates a false target RCS of greater than 30m² and using the PPI-26 thermite based flare with a minimum burn time of 3 seconds. and SOS-3-4 OWS, KKO-15LP digital full ECLSS)


(98 model adds L-150/SPO-32 Pastel 3rd Generation fully digital RHAWS with 16 targets tracked and 128> preprogrammed threat identifiers with guidance of up to 6 ARMs with 2 fired simultaneous and 10× receivers enabling a self protection envelope of 360° in azimuth and ±60° in elevation with band coverage of 1.2-18 GHz with a signal detectability range up to 320 km, BVP-60-25 1st Generation IRCM and 2nd gen RFCM with up to 120 chaff and flares)


Electronic Warfare: Options for Siren jamming Pods. 


(ML models add Options for Gvozdika jamming Pods)


Active Jamming Pods 


SPS-141 Siren 1st Generation analogue electronic active jamming with noise jamming ECM with a cassegrain antenna ECM transmitters enabling an active jamming range of 70 km>.


SPS-142 Siren 1st Generation analogue electronic active jamming with deception jamming and noise jamming ECM with a cassegrain antenna ECM transmitters enabling an active jamming range of 100 km>.

SPS-143 Siren 1st Generation analogue electronic active jamming with deception jamming and noise jamming ECM and track breaking ELINIT with cassegrain antenna ECM transmitters enabling an active jamming range of 150 km>.


Active Jamming Pods for 23ML, P & MLD 

SPS-141MVG Gvozdika 2nd Generation solid state active jamming pod operating on 8.3-10.4 GHz with deception jamming, noise jamming, sweep jamming, pulse jamming, base jamming, cross eye jamming and spot jamming ECM with track breaker and false target generation ELINIT utilising planar spiral antenna ECM transmitters for an active jamming range of 200 km>. 


Guns: GSh-23L 23mm autocannon slaved to radar with an effective firing range up to 1 km. 


Ordinance Capacity: 6× hardpoints with a max 2000 kg munition capacity and 200 rounds for the gun. 


Common Air to Air Payloads

● 4× PBP-2-3S racks with R-3S 2× APU-60-II dual racks with R-60 


R-3R 

2nd Generation Radar Missile 

PARG-13VV Conical Scanning Continuous Wave J band Semi Active Seeker with an analogue electronic parabolic cassegrain antenna array utilising a solid fuel rocket motor with a radio proximity fuse with a continuous rod warhead enabling a blast radius of 6-8 m²

~20 km max Range at 5 km+ altitude 

~10 km max Range at sea level 

~5 km engagement range vs RCS of 10m² at sea level 

~10 km engagement range vs RCS of 10m² at 5 km+ altitude 

~1 km NEZ range vs RCS of 10m² at 5 km> altitude

~Mach 2 at 5 km+ altitude 

~Mach 1 at sea level 

~Targeting Angles 40°

~Turn Rate 12 to 15 Deg/s

~Initial Acceleration of 200-300 m/s>

~20g Overload Tolerance 

~3g launch limiter 

~4g target limiter 


R-3TM

2nd Generation IR Missile 

TGS-3T3 LN² Cooled analogue electronic PIR channel Conical Scanning PbS Seeker

~15 km max Range at altitude 

~10 km max Range at sea level 

~6 km engagement range 

~Side aspect lock range 1 km

~Rear aspect lock range 3 km

~Flare Resistance 0.2

~Mach 2 at high altitude 

~Mach 1 at sea level 

~Rectile Speed: 70 Hz

~Gimbal limit: 30°

~Angular Tracking: 15 deg/s 

~Turn Rate 12 to 15 Deg/s

~Initial Acceleration of 200-300 m/s>

~Launch limiter 4g 

~Target limiter 5g 

~Overload Tolerance 20g



M model adds 


Common Air to Air Payloads

● 6× APU-23-1 racks with 4x R-23R and 2x R-23T

● 4× APU-23-1 racks with 4x R-23R 2× APU-60-II dual racks with R-60

● 5× APU-23-1 racks with 3x R-23R and 2x R-23T 1× SPS-141

● 4× APU-23-1 racks with 4x R-23R 1× APU-60-II dual racks with R-60 1× SPS-143

 

R-23T 

3rd Generation IR Missile 

TGS-23 LN² Cooled solid state MIR channel Conical Scanning InAs Seeker

~30 km max Range at altitude 

~20 km max Range at sea level 

~20 km engagement range 

~All aspect lock range 2 km

~Rear aspect lock range 10 km

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Rectile Speed: 70 Hz

~Gimbal limit: 60°

~Angular Tracking: 12 deg/s 

~Turn Rate 10 to 20 Deg/s

~Initial Acceleration of 200-300 m/s>

~Flare Resistance 0.2

~Launch limiter 4g 

~Target limiter 7g 

~Overload Tolerance 30g


R-23R

3rd Generation Radar Missile 

RGS-23 Inverse Monopulse J band Semi Active Seeker with a solid state inverse radiator cassegrain antenna array with back up inertial operting guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a radio proximity fuse with a continuous rod warhead enabling a blast radius of 8-10 m²

~50 km max Range at 10 km+ altitude 

~40 km max Range at 5 km+ altitude 

~20 km max Range at sea level 

~10 km engagement range vs RCS of 5m² at sea level 

~30 km engagement range vs RCS of 5m² at 5 km+ altitude 

~40 km engagement range vs RCS of 5m² at 10 km+ altitude 

~2 km NEZ range vs RCS of 5m² at sea level 

~10 km NEZ range vs RCS of 5m² at 5 km> altitude 

~15 km NEZ range vs RCS of 5m² at 10 km> altitude

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Targeting Angles 40°

~Turn Rate 10 to 20 Deg/s

~Initial Acceleration of 200-300 m/s>

~Launch limiter 4g 

~Target limiter 7g 

~Overload Tolerance 30g


R-60

2nd Generation IR Missile 

OGS-60TI Komar analogue electronic MWIR channel Conical Scanning PbSe Seeker

~12 km max Range 

~12 km max Range at sea level 

~8 km engagement range 

~Side aspect lock range 1 km

~Rear aspect lock range 5 km

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Rectile Speed: 100 Hz

~Flare Resistance 0.2

~Gimbal limit: 12°

~Angular Tracking: 35 deg/s 

~Turn Rate 60 to 90 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 8g 

~Target limiter 12g 

~Overload Tolerance 42g 


Bunker Busters 

BETAB-500SHP 1st Generation bunker buster

BETAB-500 1st Generation Bunker buster 

BETAB-500Y 1st Generation Bunker buster 


Unguided Bombs 

FAB-250 Unguided HE Bomb 

FAB-500 Unguided HE Bomb 

OFAB-150 Unguided Frag Bomb 

OFAB-250 Unguided Frag Bomb 

OFAB-500 Unguided Frag Bomb 

PLAB-250-120 Unguided ASW bomb 

ZAB-100-105 Unguided Incendiary bomb

ZAB-250-200 Unguided Incendiary bomb 

ODAB-500 Unguided fuel air bomb 

PTAB-500 Unguided anti tank bomb 

PTAB-500Y Unguided Anti Tank bomb 


Air to Ground Missiles 

Kh-23 2nd Generation Ballistic Missile 


UB-16-57 Rocket Pod

S-5M HE-FRAG Rocket 

S-5K HEAT Rocket 

S-5S Flechette Rocket 


B-8M1 Rocket Pod

S-8DM FAE Rocket

S-24 HE-FRAG Rocket 



ML/P/MLD models add 


Common Air to Air Payloads 

● 6× APU-23M1E racks with 4x R-24R and 2x R-24T

● 4× APU-23M1E racks with 4x R-24R 2× APU-60-II dual racks with R-60M 

● 5× APU-23M1E racks with 3x R-24R and 2x R-24T 1× SPS-141MVG 

● 4× APU-23M1E racks with 4x R-24R 1× APU-60-II dual racks with R-60M 1× SPS-141MVG 


Common Air to Ground Payloads 

4× Kh-23 2× R-24T/R-60M

2×3 FAB-250 2× R-24T/R-60M

4×16 UB-16-57 2× R-24T/R-60M

4× S-24 2× R-24T/R-60M

2×20 B-8M1 2× Kh-23 2× R-24T/R-60M


R-24T 

3rd Generation IR Missile 

TGS-23T4 LN² Cooled solid state MIR channel Conical Scanning InAs Seeker

~50 km max Range at altitude 

~30 km max Range at sea level

~30 km engagement range 

~All aspect lock range 4 km

~Rear aspect lock range 15 km

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Flare rejection 0.4

~Rectile Speed: 100 Hz

~Gimbal limit: 60°

~Angular Tracking: 20 deg/s 

~Turn Rate 10 to 20 Deg/s

~Initial Acceleration of 200-300 m/s>

~Launch limiter 4g 

~Target limiter 7g 

~Overload Tolerance 30g


R-24R

3rd Generation Radar Missile 

RGS-24 Inverse Monopulse J band Semi Active Seeker with a solid state inverse radiator cassegrain antenna array with back up inertial operting guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a radio proximity fuse and back up impact detonation with a continuous rod warhead enabling a blast radius of 10-15 m²

~70 km max Range at 10 km+ altitude 

~60 km max Range at 5 km+ altitude 

~30 km max Range at sea level 

~20 km engagement range vs RCS of 5m² at sea level 

~50 km engagement range vs RCS of 5m² at 5 km+ altitude 

~60 km engagement range vs RCS of 5m² at 10 km+ altitude 

~6 km NEZ range vs RCS of 5m² at sea level 

~15 km NEZ range vs RCS of 5m² at 5 km> altitude

~20 km NEZ range vs RCS of 5m² at 10 km> altitude

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Targeting Angles 40°

~Turn Rate 10 to 20 Deg/s

~Initial Acceleration of 200-300 m/s>

~Launch limiter 4g 

~Target limiter 7g 

~Overload Tolerance 30g


R-60M

3rd Generation IR Missile 

OGS-75 Komar-M thermoelectric Cooled digital MWIR channel Conical Scanning PbSe Seeker

~12 km max Range at altitude 

~12 km max Range at sea level 

~8 km engagement range 

~All aspect lock range 2 km

~Rear aspect lock range 8 km

~Mach 3 at high altitude 

~Mach 2 at sea level 

~Flare rejection 0.4

~Rectile Speed: 120 Hz

~Gimbal limit: 17°

~Angular Tracking: 35 deg/s 

~Turn Rate 60 to 90 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 8g 

~Target limiter 12g 

~Overload Tolerance 42g 



23-90 models add 



R-77

4th Generation Radar Missile 

9P-1348 Inverse Monopulse X band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a radio correction data link with back up inertial operting guidance, home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a Z23nA radio proximity fuse and back up impact detonation with with a high explosive blast warhead enabling a blast radius of 10-15 m²

~150 km max Range at 10 km+ altitude 

~120 km max Range at 5 km+ altitude 

~58 km max Range at seal level 

~35 km engagement range vs RCS of 5m² at sea level 

~80 km engagement range vs RCS of 5m² at 5 km+ altitude 

~110 km engagement range vs RCS of 5m² at 10 km+ altitude 

~15 km NEZ range vs RCS of 5m² at sea level 

~25 km NEZ range vs RCS of 5m² at 5 km> altitude

~30 km NEZ range vs RCS of 5m² at 10 km> altitude

~6 km ARH lock range vs RCS of 1m²

~18 km ARH lock range vs RCS of 5m²

~24 km ARH lock range vs RCS of 10m²

~0.1 m² minimum target RCS for ARH lock 

~Mach 4 at 5 km+ altitude 

~Mach 3 at sea level 

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~50g Overload Tolerance 

~8g launch limiter

~10g target limiter 


R-27ER

3rd Generation Radar Missile 

9B-1101E Inverse Monopulse X band Semi Active Seeker with a fully digital phase comparison antenna array with an INS utilising a radio correction data link with back up inertial operting guidance and polarisation filtering ECCM utilising a solid fuel rocket motor with a radio proximity fuse and back up impact detonation with a continuous rod warhead enabling a blast radius of 10-15 m²

~130 km max Range at 10 km+ altitude 

~110 km max Range at 5 km+ altitude 

~55 km max Range at sea level 

~40 km engagement range vs RCS of 5m² at sea level 

~70 km engagement range vs RCS of 5m² at 5 km+ altitude 

~90 km engagement range vs RCS of 5m² at 10 km+ altitude 

~10 km NEZ range vs RCS of 5m² at sea level 

~20 km NEZ range vs RCS of 5m² at 5 km> altitude

~30 km NEZ range vs RCS of 5m² at 10 km> altitude

~Mach 5 at 10 km+ altitude 

~Mach 4 at 5 km+ altitude 

~Mach 3 at sea level 

~Targeting Angles 35°

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~40g Overload Tolerance 

~8g launch limiter 

~10g target limiter 


R-27ET 

4th Generation IR Missile 

Geofizika-36TE LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~120 km max Range at altitude 

~40 km max Range at sea level 

~80 km engagement range 

~All aspect lock range 20 km

~Rear aspect lock range 30 km

~Mach 4 at 10 km+ altitude 

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Rectile Speed: 125 Hz

~Flare rejection 0.6

~Gimbal limit: 55°

~Angular Tracking: 60 deg/s 

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 40g 


R-74

4th Generation IR Missile 

Mayak-80B LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~30 km max Range at altitude 

~20 km max Range at sea level 

~20 km engagement range 

~All aspect lock range 6 km

~Rear aspect lock range 10 km

~Mach 3 at high altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.6

~TVC: Yes turns 180° / 3 seconds 

~Gimbal limit: 60°

~Angular Tracking: 60 deg/s 

~Turn Rate 90 to 120 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 60g 


Laser Guided Bombs 

KAB-500L 1st Generation LG HE  

KAB-500L-Pr-E 2nd Gen Bunker Buster 

KAB-500L-F-E 1st Generation FRAG-HE 

KAB-500L-OD-E 1st Generation FAE 

KAB-500L-K-E 1st Generation Cluster Bomb 


Optically Guided Bombs 

KAB-500Kr 2nd Generation HE

KAB-500Kr-Pr-E 2nd Gen Bunker Buster 

KAB-500Kr-F-E 2nd Generation FRAG-HE 

KAB-500Kr-OD-E 2nd Generation FAE 

KAB-500Kr-K-E 2nd Generation Cluster Bomb


Air to Ground Missiles 

Kh-59-M 3rd Generation HE Cruise Missile

Kh-59-K 3rd Generation HEAT Cruise Missile

Kh-59-KE 3rd Gen Cluster Cruise Missile

Kh-59L-M 2nd Gen Laser Guided HE

Kh-59L-K 2nd Gen Laser Guided HEAT

Kh-59L-KE 2nd Gen Laser Guided Cluster 

Kh-59T-M 2nd Generation OG HE

Kh-59T-K 2nd Generation OG HEAT

Kh-59T-KE 2nd Generation OG Cluster 

Kh-29T-M 2nd Generation OG HE

Kh-29T-K 2nd Generation OG HEAT 

Kh-29L-M 2nd Generation Laser Guided HE 

Kh-29L-K 2nd Generation Laser Guided HEAT 



MiG-23S


MiG-23M


MiG-23ML



MiG-23MLA 

MiG-23P


MiG-23MLD


MiG-23-98






MiG-21 Fishpot Family 


MiG-21F 

Designed: 1952

Prototype: 1955

Completed: 1956

Production: 1958

Service: 1960

Generation: 2nd 

Aircraft Role: Fighter

Number Made: 1000+

Combat Rank: S


MiG-21PF 

Designed: 1958

Prototype: 1960

Completed: 1962

Production: 1962

Service: 1964

Generation: 2+

Aircraft Role: Interceptor/Fighter

Number Made: 5000+

Combat Rank: S


MiG-21PFM 

Designed: 1962

Prototype: 1964

Completed: 19664

Production: 1964

Service: 1965

Generation: 2+

Aircraft Role: Interdictor/Fighter

Number Made: 3000+

Combat Rank: S


MiG-21S

Designed: 1962

Prototype: 1964

Completed: 1964

Production: 1965

Service: 1968

Generation: 3rd

Aircraft Role: Interceptor/Fighter

Number Made: 6000+

Combat Rank: S


MiG-21SMT

Designed: 1965

Prototype: 1966

Completed: 1968

Production: 1969

Service: 1970

Generation: 3rd

Aircraft Role: Interceptor/Fighter

Number Made: 1000+

Combat Rank: S


MiG-21R

Designed: 1964

Prototype: 1965

Completed: 1966

Production: 1967

Service: 1968

Generation: 2+

Aircraft Role: Interceptor/Fighter

Number Made: 300+

Combat Rank: S


MiG-21bis

Designed: 1968

Prototype: 1971

Completed: 1972

Production: 1973

Service: 1975

Generation: 3rd

Aircraft Role: Fighter

Number Made: 4,000+

Combat Rank: S


MiG-21-93

Designed: 1994

Prototype: 1995

Generation: 4th

Aircraft Role: Interdictor/Fighter

Number Made: 10+

Combat Rank: D


Engine and Airframe: All metal construction with an RCS minimum of 2m². Crew of 1. Length 14.7 m. Height 4.1 m. Wingspan 14 m. Wing area 23 m². Frame weight 7,000 kg. Takeoff weight 10,400 kg. Max Fuel 2,000 kg.  1× Tumansky Axial flow R-25-300 turbojet with 40 kN of thrust and 70 kN in afterburner. Sustained G tolerance of 5g and a max Overload Tolerance of 9g. Wing loading 300-360 kg/m²


Speed and Endurance: Top speed of mach 1.8 to 2 at 15 km+, mach 1.5 to 2 at 10 km+, mach 1.4 to 1.8 to at 5 km+ and mach 1 to 1.1 at sea level. Service Ceiling of 17 to 19 km. Combat range of 600-800 km. Acceleration 15-19 seconds to mach 1 at sea level. Stall speed 220-300 kph. 


(S model adds R11-F2S-300 turbojet with 48 kN of thrust and 76 kN in afterburner. Top speed of mach 2 to 2.2 at 15 km+, mach 1.8 to 2 at 10 km+, mach 1.5 to 1.8 to at 5 km+ and mach 1 to 1.3 at sea level)


(SMT model adds R-13F-300 axial flow turbojet)


(R model adds R-11F2S-300 axial flow turbojet with an analogue electronic engine control)


(Bis adds R-25-300 turbojet axial flow turbojet with an analogue electronic engine control)


(93 model adds R25-300M axial flow turbojet with an digital electronic engine control)


Manuvarabilities: Thrust to weight ratio of 0.7 at full air to air payload and 1 at half fuel/loadout. Roll rate of 240 deg/s at high speed and 300 deg/s at low speed. Climb rate of 140-170 m/s. Angle of Attack at 14° at mach 2>, 20° at mach 1> and 25° at mach <1. 20 to 160 kph/s speed bleed at high g instantaneous maneuvers and 30 to 110 kph/s speed bleed at high g sustained maneuvers


(S model onwards adds Climb rate of 170-200 m/s. Thrust to weight ratio of 1 at full air to air payload and 1.3 at half fuel/loadout)


Aircraft Turn Rates 


Sustained turn rates 


Mach ~1.5 Speeds 

● 1-2 deg/s at sea level 


Mach ~1 Speeds 

● 4-5 deg/s at 10 km altitude 

● 6-8 deg/s at 5 km altitude 

● 9-12 deg/s at sea level 


Mach ~0.5 Speeds 

● 7-9 deg/s at 10 km altitude 

● 10-13 deg/s at 5 km altitude 

● 13-17 deg/s at sea level 


Instantaneous turn rates 


Mach ~1.5 Speeds 

● 4-7 deg/s at sea level 


Mach ~1 Speeds 

● 2-4 deg/s at 10 km altitude 

● 9-11 deg/s at 5 km altitude 

● 13-17 deg/s at sea level  


Mach ~0.5 Speeds 

● 4-7 deg/s at 10 km altitude 

● 9-13 deg/s at 5 km altitude 

● 14-19 deg/s at sea level  


Airframe RCS

RCS Minimum: 2m²

RCS Median: 3m²

RCS Average: 4-6m²


Navigation & Flight Control: Analogue flight control system. BU-6 hydromechanical AFCS with an SVS-6 triode ADC. 1st Generation cockpit. ARK-5 analogue ADF. ZSh-3 Flight Helmet. RSBN-2S Svod analogue electronic radio navigation system. 


(PFM model adds ARK-10 analogue ADF)


Fire Control: S-11 analogue FCS utilising triodes. SRD-5M Baza-6 Rangefinding Radar. ASP-5NV-U1 1st Generation HUD with an analogue electronic CRT collimator reflector utilising rangefinding radar


(Early PF model used RP-9-21 TsD-30Š¢-21 1st Generation tracking radar) 


(PF model adds S-13 analogue FCS with RS-2-US radar targeting. RP-21 TsD-30TP 1+ Generation analogue electronic mechanically steered J band connical scanning radar system with an inverse radiator cassegrain antenna array with analogue signal processing, A, B and C scope radar image displayed with CW illumination for SARH guidance with multi mode operating function and conical and spiral scan scanning modes utilising SRC and STTR air to air radar modes with gain modulation ECCM with LPRF power output on average being 100-200 W with a 20 kW max output with a 520 mm antenna diameter. ASP-5NV-U1 1st Generation HUD with an analogue electronic CRT collimator reflector utilising rangefinding radar. 2nd Generation Radar display with a CRT screen utilising a A oscilloscope for target engagement and a B oscilloscope for target search. RSBN-4S Iskra-K analogue electronic radio navigation system)


(PFM model adds S-21M analogue FCS with RS-2-US radar targeting. RP-21MA TsD-30TPM 1+ Generation analogue electronic mechanically steered J band connical scanning radar system with a inverse radiator cassegrain antenna array with analogue signal processing, A, B and C scope radar image displayed with CW illumination for SARH guidance and IFF integration with multi mode operating function and conical and spiral scan scanning modes utilising SRC and STTR air to air radar modes with gain modulation ECCM with LPRF power output on average being 100-200 W with a 20 kW max output with a 520 mm antenna diameter. VB-21 mechanical ballistic computer with semi automatic analogue target lead with a max gun accuracy, whilst flying up to 300 kph, under 1 MRAD up to 300m and under 0.5 MRAD up to 200m and bomb and rocket accuracy of <100-300m CEP at a range up to 2000m and altitudes up to 3000m and <900-1500m CEP at a range up to 10,000m and altitude up to 12,000m. RS-2-US radar beam riding MCLOS system)


(93 model adds Kopyo fully computerised FCS utilising Ts-101 digital FCC utilising K1801 16x bit CPUs performing 300-400k IPS and 150-200m FLOPS. Kopyo-21 3rd Generation digital X band pulse doppler radar with a mechanically steered slotted planar array with power output on average being 1-2 kW with a 4 kW max output with a 520 mm antenna. TsVBM-93 digital ballistic computer utilising a KM1810VM88 16x bit CPU enabling automatic digital target lead with gun, rocket and bomb CCRP and CCIP with a max bomb and rocket accuracy of <10-20m CEP at a range up to 2000m and altitudes up to 3000m and <100-300m CEP at a range up to 10,000m and altitude up to 10,000m. R-800 and R-862 VHF/UHF and R-864 HF Digital radios. ZSh-7 Helmet with Shchel-3UM1 1st Generation HMD. ILS-31 4th Generation fully digital HUD with an integrated digital bombing complex with gun, bomb and rocket CCRP and CCIP with full gun EEGS. 4th Generation Radar display with an SVD system utilising a CRT display with a polychrome raster image)


(S models add BU-51M hydromechanical AFCS with an SVS-21S nuvistor ADC. S-21 electromechanical FCS with angle of slide, angle of attack, air speed, altitude and aircraft position computed with analogue systems with RLPK-22 radar targeting, RP-22S Sapfir-21 2nd Generation mechanically steered J band analogue electronic monopulse radar system with a C band beacon interrogator with an inverse radiator cassegrain antenna array with analogue signal processing, P, K, E and C scope radar image displayed with CW illumination for SARH guidance and IFF integration with multi mode operating function and raster, conical, and spiral scan scanning modes utilising SRC, STTR and RFR ACM air to air radar modes with gain modulation and polarization filtering ECCM with a LPRF power output on average being 100-200 W with a 40 kW max output with a 520 mm antenna diameter. ASP-PF-21 2nd Generation HUD with an analogue electronic CRT collimator reflector utilising a rangefinding radar with velocity, boresight, acceleration, pitch, barometric, heading, altitude and speed displayed with gun, bomb and rocket CCRP and CCIP. ITO-1 3rd Generation Radar display with a CRT screen utilising a K/E oscilloscope for target engagement and a P/C oscilloscope for target search. R-802G analogue radio. RV-4 radar altimeter, ARK-10 analogue ADF, RSBN-5S analogue electronic radio navigation system with APP-155 3× axis electromechanical autopilot. AVM-21 electromechanical ballistic computer enabling gun and missile coursing)


(SM and SMT model adds S-21 electromechanical FCS with angle of slide, angle of attack, air speed, altitude and aircraft position computed with analogue systems with RLPK-22 radar targeting, RP-22SM Sapfir-21M 2nd Generation mechanically steered J band analogue electronic monopulse radar system with a C band beacon interrogator with a inverse radiator cassegrain antenna array with analogue signal processing, P, K, E and C scope radar image displayed with CW illumination for SARH guidance and IFF integration with multi mode operating function and raster, conical, and spiral scan scanning modes utilising SRC, STTR and RFR ACM air to air radar modes with gain modulation and polarization filtering ECCM with LPRF power output on average being 100-200 W with a 40 kW max output with a 520 mm antenna diameter)


(Bis model adds S-22 electromechanical FCS with angle of slide, angle of attack, air speed, altitude and aircraft position computed with analogue systems with RLPK-22S radar targeting, RP-22SMA Sapfir-21M 2nd Generation mechanically steered J band analogue electronic monopulse radar system with a C band beacon interrogator with a inverse radiator cassegrain antenna array with analogue signal processing, P, K, E and C scope radar image displayed with CW illumination for SARH guidance and IFF integration with multi mode operating function and raster, conical, and spiral scan scanning modes utilising SRC, STTR and RFR ACM air to air radar modes with gain modulation and polarization filtering ECCM with LPRF power output on average being 100-200 W with a 40 kW max output with a 520 mm antenna diameter)


Communication & C2: RSIU-3 VHF analogue electronic radio with two way communication operating on 6 pre set channels with a 120 km communication range and the Gorizont-1 analogue electronic command Data link with automated GCI.


(PF model onwards add Klyon analogue electronic communication system with the RSIU-4V VHF analogue electronic radio with 2 way communication, FM and AM receiving and built in IAD with voice formats with 20 pre set channels with an operating communication range of 200 km)


Targeting: SRD-5M ranging radar with max engagement range up to 2 km. 


(Early PF model adds TsD-30Š¢-21 radar with a horizontal scan range of 60° and ±10° vertical scan range enabling a track range of 15 km for an aircraft with an RCS of 16m² with max tracking target velocity at over 2500 kph)


(PF model adds TsD-30TP radar with a horizontal scan range of 60° and ±10° vertical scan range enabling a track range of 17 km for an aircraft with an RCS of 16m² with max tracking target velocity at over 2500 kph) 


(PFM model adds TsD-30TPM radar with a horizontal scan range of 60° and ±10° vertical scan range enabling a track range of 20 km for an aircraft with an RCS of 16m² with max tracking target velocity at over 2500 kph)


(S models add Sapfir-21 radar with a horizontal scan range of 60° and ±10° vertical scan range enabling an Rmax range up to 30 km, with a detection range of 20 km for 16m² and a track range of 10 km for an aircraft with an RCS of 16m² with a rangefinding radar gun engagement range up to 2 km with a tracking scan range of 30° in azimuth and -6°/+6° in elevation with a scan sweep in 3 to 5 seconds with max tracking target velocity at over 2500 kph)


(SM and SMT model adds Sapfir-21M radar with a horizontal scan range of 60° and ±10° vertical scan range enabling an Rmax range up to 30 km, with a detection range of 23 km for 16m² and a track range of 13 km for an aircraft with an RCS of 16m² with a rangefinding radar gun engagement range up to 2 km with a tracking scan range of 30° in azimuth and -6°/+6° in elevation with a scan sweep in 3 to 5 seconds with max tracking target velocity at over 2500 kph)


(bis model adds Sapfir-21MA radar with a horizontal scan range of 60° and ±10° vertical scan range enabling an Rmax range up to 30 km, with a detection range of 25 km for 16m² and a track range of 17 km for an aircraft with an RCS of 16m² with a rangefinding radar gun engagement range up to 2 km with a tracking scan range of 30° in azimuth and -6°/+6° in elevation with a scan sweep in 3 to 5 seconds with max tracking target velocity at over 2500 kph)


(93 model adds Kopyo-21 pulse doppler radar with 60° horizontal and -10°/+10° vertical scan range enabling tracking of up to 8 targets and locking of 2 with an Rmax range up to 90 km, detection range of 70 km for 3m² and a 45 km track range for an aircraft with an RCS of 3m² with a horizontal SNP scan range of 40° and a horizontal SNP scan time of 2 seconds with max tracking target velocity at over 3000 kph and stores tracking information for up to 2 non tracked target with predictive flight paths for non tracked targets up to 10 seconds. Shchel-3UM1 HMD with a 140° horizontal FOV and -30°/+30° vertical FOV utilising automatic cueing for targeting with head tracking software)


(Some MIG-21Fs from 1958 onwards added the SIV-52 Generation 0 IRST utilising a thermoelectric cooled spin scan PbS analogue electronic signal detector with a max detection range up to 10 km with a 4 to 8 km detection range for bomber sized aircraft with a 0.5 to 1.2 km detection range for fighter sized aircraft with a horizontal FOV up to 14° and a vertical FOV of -2°/+5°)


(Some MiG-21S models starting from 1968 were fitted with IVP-2 Samotsvet low definition LLLTV system that had a detection range of 2 to 14 km depending on target size and conditions) 


Counter Measures: SPO-2B Sirena-2B Generation 0 analogue electronic RWR with 3 targets tracked with a single receiver enabling a self protection envelope of 180° in azimuth and ±20° in elevation with band coverage of 6-20 GHz. SSP analogue fire warning system. KM-1 ejection seat. KKO-3 analogue electronic ECLSS. SO-57/SRZO-2 1st Generation analogue electronic IFF interrogator / transponder linked to the Kremnij-2 unsecured analogue electronic IFF system with aircraft ID.


(R model adds SPO-3 Sirena-3 1st Generation analogue electronic RWR with 4 targets tracked with 4× receivers enabling a self protection envelope of 360° in azimuth and ±90° in elevation with band coverage of 6-20 GHz) 


(S, SMT and Bis model adds SPO-10 Sirena-3M 1st Generation solid state RWR with 4 targets tracked with 4× receivers enabling a self protection envelope of 360° in azimuth and ±90° in elevation with band coverage of 6-20 GHz, SSP-1 analogue electronic fire countermeasure system, CU32-SORC analogue ICAS and KKO-5LP solid state full ECLSS. SO-57M/SRZO-2M 1st Generation analogue electronic IFF interrogator / transponder linked to the Kremnij-2M2 analogue electronic secure IFF system with aircraft ID and basic data encryption)


(S model onwards had options for ASO-2I countermeasure dispenser utilising 1st Generation IRCM and RFCM with 68 total rounds using the PPR-26-13 composite aluminium chaff that activates in 0.3 seconds and creates a false target RCS of greater than 30m² and using the PPI-26 thermite based flare with a minimum burn time of 3 seconds)


(93 model adds L-150/SPO-32 Pastel 3rd Generation fully digital RHAWS with 16 targets tracked and 128> preprogrammed threat identifiers with guidance of up to 6 ARMs with 2 fired simultaneous and 10× receivers enabling a self protection envelope of 360° in azimuth and ±60° in elevation with band coverage of 1.2-18 GHz with a signal detectability range up to 320 km. BVP-21 1st Generation IRCM and RCM with 60 chaff and flares)


Electronic Warfare: N/A


(PF model onwards adds options for Siren jamming Pods)


Active Jamming Pods for PF models onwards 


SPS-141 Siren 1st Generation analogue electronic active jamming with noise jamming ECM with a cassegrain antenna ECM transmitters enabling an active jamming range of 70 km>.


SPS-142 Siren 1st Generation analogue electronic active jamming with deception jamming and noise jamming ECM with a cassegrain antenna ECM transmitters enabling an active jamming range of 100 km>.


SPS-143 Siren 1st Generation analogue electronic active jamming with deception jamming and noise jamming ECM and track breaking ELINIT with cassegrain antenna ECM transmitters enabling an active jamming range of 150 km>.



Pods for MiG-21R 

Type R Pod with SRS-6/7 Romb-4A/B analogue electronic SIGNIT system. 
Prostor Pod with 1st Generation IRLS system. 
Sphil-1 laser imaging system. 


Guns: GP-9 23mm autocannon slaved to radar with an effective firing range up to 1 km. (Needs hardpoint)


(PFM, S and R models add GSh-23L 23mm internal autocannon slaved to radar) 


Ordinance Capacity: 5× hardpoints with a max 2000 kg munition capacity with 200 rounds for the gun. 


(PFM, S and R  model uses 4× hardpoints)


Common Payloads 

4×16 UB-16-57 1× GP-9


UB-16-57 Rocket Pods 

S-5 KEP

S-5M HE-FRAG

S-5S Flechette 

S-5P Chaff 


PF models add


Common Air to Air Payloads: 

● 2× C-1-U racks with RS-1U 2× APU-13 racks with R-3T



RS-1U

1st Generation Radar Missile 

K-5 Radar Beam riding Seeker

~6 km Range 

~Mach 2 speed 


R-3T

1st Generation IR Missile 

TGS-3 analogue electronic PIR channel Conical Scanning PbS Seeker

~10 km max Range at altitude 

~10 km max Range at sea level 

~6 km engagement range 

~Rear aspect lock range 1 km

~Mach 2 at 5 km+ altitude 

~Mach 1 at sea level 

~Rectile Speed: 50 Hz

~Gimbal limit: 28°

~Angular Tracking: 10 deg/s 

~Launch limiter 4g 

~Target limiter 5g 

~Overload Tolerance 15g


PFM model adds 

B-13L Rocket Pod

S-5M HE-FRAG Rocket 

S-5K HEAT Rocket 

S-5S Flechette Rocket 


B-8M1 Rocket Pod

S-8S Flechette rocket 

S-8P chaff rocket 

S-8D FAE rocket 

S-8KO HEAT Rocket 

S-8B Bunker buster rocket 


Unguided Bombs 

OFAB-150 Unguided Frag Bomb 

OFAB-250 Unguided Frag Bomb 

PLAB-250-120 Unguided ASW bomb 

FAB-250 Unguided HE Bomb 


Air to Ground Missiles 

Kh-66 2nd Generation Land attack ballistic missile


S and R models Add following 


Common Air to Air Payloads 

● 4× APU-13U-2 racks with 2× R-3S and 2× R-3T 


R-3R 

2nd Generation Radar Missile 

PARG-13VV Conical Scanning Continuous Wave J band Semi Active Seeker with an analogue electronic parabolic cassegrain antenna array utilising a solid fuel rocket motor with a radio proximity fuse with a continuous rod warhead enabling a blast radius of 6-8 m²

~20 km max Range at 5 km+ altitude 

~10 km max Range at sea level 

~5 km engagement range vs RCS of 10m² at sea level 

~10 km engagement range vs RCS of 10m² at 5 km+ altitude 

~1 km NEZ range vs RCS of 10m² at 5 km> altitude

~Mach 2 at 5 km+ altitude 

~Mach 1 at sea level 

~Targeting Angles 40°

~Turn Rate 12 to 15 Deg/s

~Initial Acceleration of 200-300 m/s>

~20g Overload Tolerance 

~3g launch limiter 

~4g target limiter 


R-3TM

2nd Generation IR Missile 

TGS-3T3 LN² Cooled analogue electronic PIR channel Conical Scanning PbS Seeker

~15 km max Range at altitude 

~10 km max Range at sea level 

~6 km engagement range 

~Side aspect lock range 1 km

~Rear aspect lock range 3 km

~Flare Resistance 0.2

~Mach 2 at high altitude 

~Mach 1 at sea level 

~Rectile Speed: 70 Hz

~Gimbal limit: 30°

~Angular Tracking: 15 deg/s 

~Turn Rate 12 to 15 Deg/s

~Initial Acceleration of 200-300 m/s>

~Launch limiter 4g 

~Target limiter 5g 

~Overload Tolerance 20g


bis model and later S models add


● 2× PBP-2-3S racks with R-3S 2× APU-60-II dual racks with R-60 


R-60

2nd Generation IR Missile 

OGS-60TI Komar analogue electronic MWIR channel Conical Scanning PbSe Seeker

~12 km max Range 

~12 km max Range at sea level 

~8 km engagement range 

~Side aspect lock range 1 km

~Rear aspect lock range 5 km

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Rectile Speed: 100 Hz

~Flare Resistance 0.2

~Gimbal limit: 12°

~Angular Tracking: 35 deg/s 

~Turn Rate 60 to 90 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 8g 

~Target limiter 12g 

~Overload Tolerance 42g 



21-93 models add 


Common Air to Air Payloads 

2× R-77 2× R-73M/R-27ET

2× R-27ER 2× R-73M/R-27ET


Common Air to Ground Payloads 

1× Kh-59 1× Kh-29 2× R-73M/R-27ET

1× KAB-500Kr 1× KAB-500L 2× R-73M/R-27ET


R-77

4th Generation Radar Missile 

9P-1348 Inverse Monopulse X band Active Seeker with a fully digital slotted planar antenna array with an INS utilising a radio correction data link with home on jam and polarisation filtering ECCM utilising a solid fuel rocket motor with a Z23nA radio proximity fuse and back up impact detonation with with a high explosive blast warhead enabling a blast radius of 10-15 m²

~150 km max Range at 10 km+ altitude 

~120 km max Range at 5 km+ altitude 

~58 km max Range at seal level 

~35 km engagement range vs RCS of 5m² at sea level 

~80 km engagement range vs RCS of 5m² at 5 km+ altitude 

~110 km engagement range vs RCS of 5m² at 10 km+ altitude 

~15 km NEZ range vs RCS of 5m² at sea level 

~25 km NEZ range vs RCS of 5m² at 5 km> altitude

~30 km NEZ range vs RCS of 5m² at 10 km> altitude

~6 km ARH lock range vs RCS of 1m²

~18 km ARH lock range vs RCS of 5m²

~24 km ARH lock range vs RCS of 10m²

~0.1 m² minimum target RCS for ARH lock 

~Mach 4 at 5 km+ altitude 

~Mach 3 at sea level 

~Targeting Angles 45°

~Turn Rate 40 to 150 Deg/s

~Initial Acceleration of 240-400 m/s>

~50g Overload Tolerance 

~8g launch limiter

~10g target limiter 


R-27ER

3rd Generation Radar Missile 

9B-1101E Inverse Monopulse X band Semi Active Seeker with a fully digital phase comparison antenna array with an INS utilising a radio correction data link with polarisation filtering ECCM utilising a solid fuel rocket motor with a radio proximity fuse and back up impact detonation with a continuous rod warhead enabling a blast radius of 10-15 m²

~130 km max Range at 10 km+ altitude 

~110 km max Range at 5 km+ altitude 

~55 km max Range at sea level 

~40 km engagement range vs RCS of 5m² at sea level 

~70 km engagement range vs RCS of 5m² at 5 km+ altitude 

~90 km engagement range vs RCS of 5m² at 10 km+ altitude 

~10 km NEZ range vs RCS of 5m² at sea level 

~20 km NEZ range vs RCS of 5m² at 5 km> altitude

~30 km NEZ range vs RCS of 5m² at 10 km> altitude

~Mach 5 at 10 km+ altitude 

~Mach 4 at 5 km+ altitude 

~Mach 3 at sea level 

~Targeting Angles 35°

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~60g Overload Tolerance 

~8g launch limiter 

~10g target limiter 


R-27ET 

4th Generation IR Missile 

Geofizika-36TE LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~120 km max Range at altitude 

~40 km max Range at sea level 

~80 km engagement range 

~All aspect lock range 20 km

~Rear aspect lock range 30 km

~Mach 4 at 10 km+ altitude 

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Rectile Speed: 125 Hz

~Flare rejection 0.6

~Gimbal limit: 55°

~Angular Tracking: 60 deg/s 

~Turn Rate 20 to 40 Deg/s

~Initial Acceleration of 220-390 m/s>

~Launch limiter 8g 

~Target limiter 9g 

~Overload Tolerance 60g 


R-74

4th Generation IR Missile 

Mayak-80B LN² Cooled fully digital MIR pseudo-imaging InSb Seeker with gatewidth IRCCM

~30 km max Range at altitude 

~20 km max Range at sea level 

~20 km engagement range 

~All aspect lock range 6 km

~Rear aspect lock range 10 km

~Mach 3 at high altitude 

~Mach 2 at sea level 

~Rectile Speed: 150 Hz

~Flare rejection 0.6

~TVC: Yes turns 180° / 3 seconds 

~Gimbal limit: 60°

~Angular Tracking: 60 deg/s 

~Turn Rate 90 to 120 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 12g 

~Target limiter 12g 

~Overload Tolerance 60g 


Laser Guided Bombs 

KAB-500L 1st Generation LG HE  

KAB-500L-Pr-E 2nd Gen Bunker Buster 

KAB-500L-F-E 1st Generation FRAG-HE 

KAB-500L-OD-E 1st Generation FAE 

KAB-500L-K-E 1st Generation Cluster Bomb 


Optically Guided Bombs 

KAB-500Kr 2nd Generation HE

KAB-500Kr-Pr-E 2nd Gen Bunker Buster 

KAB-500Kr-F-E 2nd Generation FRAG-HE 

KAB-500Kr-OD-E 2nd Generation FAE 

KAB-500Kr-K-E 2nd Generation Cluster Bomb


Air to Ground Missiles 

Kh-59-M 3rd Generation HE Cruise Missile

Kh-59-K 3rd Generation HEAT Cruise Missile

Kh-59-KE 3rd Gen Cluster Cruise Missile

Kh-59L-M 2nd Gen Laser Guided HE

Kh-59L-K 2nd Gen Laser Guided HEAT

Kh-59L-KE 2nd Gen Laser Guided Cluster 

Kh-59T-M 2nd Generation OG HE

Kh-59T-K 2nd Generation OG HEAT

Kh-59T-KE 2nd Generation OG Cluster 

Kh-29T-M 2nd Generation OG HE

Kh-29T-K 2nd Generation OG HEAT 

Kh-29L-M 2nd Generation Laser Guided HE 

Kh-29L-K 2nd Generation Laser Guided HEAT 



MiG-21F


MiG-21PF 


MiG-21PFM


MiG-21S



MiG-21SMT

MiG-21bis 

MiG-21R 
MiG-21-93 




Su-15 Flaggon Family 


Su-15

Designed: 1958

Prototype: 1962

Completed: 1963

Production: 1964

Service: 1965

Aircraft Role: Interceptor 

Generation: 2+

Combat Rank: D

Number Made: 200+


Su-15T

Designed: 1964

Prototype: 1965

Completed: 1968

Production: 1969

Aircraft Role: Interceptor 

Generation: 3rd 

Combat Rank: D

Number Made: 20+


Su-15TM

Designed: 1967

Prototype: 1969

Completed: 1970

Production: 1972

Service: 1973

Aircraft Role: Interceptor 

Generation: 3rd

Combat Rank: D

Number Made: 1000+


Airframe and Engines: All metal construction with an RCS minimum of 6m². Crew of 1. Length 19.5 m. Height 4.8 m. Wingspan 9.4 m. Wing area 62 m². Frame weight 10,760 kg. Takeoff weight 17,900 kg. Max Fuel 5,330 kg  2× Tumansky R-13F-300 axial flow turbojets with 80 kN of thrust and 130 kN in afterburner. Sustained G tolerance of 5g and a max Overload Tolerance of 7g. Wing loading of 380-520 kg/m². Uu8XBBurqHg


Speed and Endurance: Top speed of mach 2.3 to 2.6 at 15 km+, mach 2.1 to 2.4 at 10 km+, mach 2 to 2.2 to at 5 km+ and mach 1 to 1.3 at sea level. Service Ceiling of 17 to 22 km. Combat Range of 400 to 600 km. Take off distance is 700m with ATA payload to 900m for full payload. Landing distance 800 to 1100m. 


Manuvarabilities: Thrust to weight ratio of 0.7 at full air to air payload and 1 at half fuel/loadout. Roll rate of 250 deg/s at high speed and 300 deg/s at low speed. Climb rate of 140-170 m/s. Angle of Attack at 18° at mach 2>, 16° at mach 1> and 15° at mach <1. Speed bleed at 50-80% at instantaneous 7g> maneuvers and 50-80% at sustained 5g> maneuvers.


Navigation & Flight Control:. BU-49 Hydromechanical AFCS with an SVS-49 nuvistor ADC. RV-4 analogue electronic radar altimeter. RSBN-5S Iskra-K analogue electronic radio navigation system with VOR with a position accuracy of 500-1200m and angular accuracy of ±4°.


(T model adds PrNK-15 analogue nav/attack system with a SAU-58 3× axis electromechanical autopilot and a BU-49 hydromechanical AFCS utilising a NVU-48 nuvistor ADC with a NK-48 solid state navigation system using an analogue INS with a TsSVS-15-49 solid state navigation computer. ZSh-3 Flight Helmet) 


Fire Control: analogue FCS. RP-15 Oryol-D58 1+ Generation analogue electronic mechanically steered J band connical scanning radar system with a C band beacon interrogator with a parabolic reflector antenna array with analogue signal processing, A, B and C scope radar image displayed with CW illumination for SARH guidance and IFF integration with multi mode operating function and conical and spiral scan scanning modes utilising SRC and STTR air to air radar modes with gain modulation ECCM with a LPRF power output on average being 120 W with a 90 kW max output with a 680 mm antenna diameter. 2nd Generation Radar display with a CRT screen utilising a A oscilloscope for target engagement and a B oscilloscope for target search. 


(T model adds S-15 electromechanical FCS with angle of slide, angle of attack, air speed, altitude and aircraft position computed with analogue systems with RLPK-26 radar targeting system. RP-26 Taifun 2nd Generation mechanically steered J band analogue electronic monopulse radar system with a C band beacon interrogator with a long chord twist cassegrain antenna array with analogue signal processing, P, K, E and C scope radar image displayed with CW illumination for SARH guidance and IFF integration with multi mode operating function and raster, conical, and spiral scan scanning modes utilising SRC, STTR and RFR ACM air to air radar modes with gain modulation and polarization filtering ECCM with a LPRF power output on average being 300 W with a 150 kW max output with a 700 mm antenna diameter. PKI-10T analogue HUD. ITO 3rd Generation Radar display with a CRT screen utilising a K/E oscilloscope for target engagement and a P/C oscilloscope for target search. 


Communication & C2:  Klyon analogue electronic communication complex with the RSIU-5V VHF analogue electronic radio with 2 way communication, FM and AM receiving and built in IAD with voice formats with 20 pre set channels with an operating communication range of 200 km. Vozdukh-1 analogue electronic GCI complex with the ARL-S Lazour-S analogue electronic navigation and command Data Link connected with the MRP-48P marker beacon, SAU-58 electromechanical autopilot, ARK-10 analogue electronic ADF, SO-57M analogue electronic IFF interrogator and the SRZO-2M analogue electronic transponder linked to the PVO Strany URAGAN air defence network with fully automated ground controlled interception, data encryption and IFF integration utilising ground and air based radar and computer generated data exchange with pre recorded sound and text formats used, with data transfer speeds of 54 bit/s every 4 to 5 enabling a LOS data transmission range up to 200 km with data exchange between 3 aircraft. 


(TM model adds S-15M electromechanical FCS with angle of slide, angle of attack, air speed, altitude and aircraft position computed with analogue systems with. RP-26M Taifun-M 2nd Generation mechanically steered J band analogue electronic monopulse radar system with a C band beacon interrogator with a long chord twist cassegrain antenna array with analogue signal processing, P, K, E and C scope radar image displayed with CW illumination for SARH guidance and IFF integration with multi mode operating function and raster, conical, and spiral scan scanning modes utilising SRC, STTR and RFR ACM air to air radar modes with gain modulation and polarization filtering ECCM with a LPRF power output on average being 150-300 W with a 150 kW max output with a 700 mm antenna diameter. Vozdukh-1M analogue electronic GCI complex with the ARL-SM Lazour-M analogue electronic navigation and command Data Link connected with the SAU-58 electromechanical autopilot, ARK-10 analogue ADF, SO-63 solid state interrogator and SRZO-2M analogue electronic IFF transponder linked to the Voyska PVO Strany URAGAN air defence network with fully automated ground controlled interception, data encryption and IFF integration utilising ground and air based radar and computer generated data exchange with pre recorded sound and text formats used, with data transfer speeds of 54 bit/s every 4 to 5 enabling a LOS data transmission range up to 350 km with data exchange between 3 aircraft)


(Later TM models add RP-26M Taifun-M2 2+ Generation J band mechanically steered solid state long chord twist cassegrain antenna arrays with a C band beacon interrogator with analogue signal processing, P, K, E and C scope radar image displayed with MTI based LDSD, CW illumination for SARH guidance and IFF integration with multi mode operating function and raster, conical, and spiral scan scanning modes utilising SRC/LDSD, STTR and IRST and RFR based ACM air to air radar modes with gain modulation and polarization filtering ECCM with a LPRF power output on average being 150-300 W with a 150 kW max output with a 700 mm antenna diameter.  Evkalipt solid state communication complex with the R-855/R-832 VHF/UHF and R-802 HF solid state radios with 2 way communication, FM and AM receiving, built in IAD and secure voice encryption with voice formats utilised operating on 120 pre set channels with an operating communication range of 300 km. Rubezh digital GCI complex with the Biryusa digital navigation data links and BAN-75, SVPK, SPK-75 and SPK-68 digital command data links connected to the SAU-58 autopilot, ARK-19 solid state ADF, SO-69 solid state IFF interrogator and SRZO-2P solid state IFF transponder linked to the PVO NDCC air defence network with fully automated ground controlled interception, weapons management, IFF integration, digital data encryption and navigation data utilising ground based computer and radar generated data exchange with pre recorded voice and text formats used with data transfer speeds of 45 bit/s, 80 bit/s and 96 bit/s every 5 to 10 seconds operating on 2 MHz to 400 MHz with up to 20,000 frequency hops per second on 20+ frequency carriers with LOS data transmission range up to 400 km and BLOS up to 1000 km with data exchange between up to 36 aircraft)


Targeting: Oryol-D58 radar with a horizontal scan range of 60° and -10°/+30° vertical scan range enabling a search range of 35 km for aircraft with an RCS of 16m² and a track range of 20 km for an aircraft with an RCS of 16m² with a tracking scan range of 30° in azimuth and -5°/+5° in elevation with a scan sweep in 3 to 6 seconds with max tracking target velocity at over 2500 kph.


(T model adds Taifun radar with a horizontal scan range of 140° and -10°/+30° vertical scan range enabling an Rmax range up to 70 km, with a look up detection range of 55 km for 16m² and a track range of 35 km for an aircraft with an RCS of 16m² with a tracking scan range of 30° in azimuth and -7°/+7° in elevation with a scan sweep in 2 to 5 seconds with max tracking target velocity at over 3700 kph) 


(TM model adds Taifun-M radar with a horizontal scan range of 140° and -10°/+30° vertical scan range enabling an Rmax range up to 70 km, with a look up detection range of 70 km for 16m² and a track range of 45 km for an aircraft with an RCS of 16m² with a tracking scan range of 30° in azimuth and -7°/+7° in elevation with a scan sweep in 2 to 5 seconds with max tracking target velocity at over 3700 kph)


(Later TM models add Taifun-M2 radar with a horizontal scan range of 140° and -10°/+30° vertical scan range enabling an Rmax range up to 90 km, with a look up detection range of 70 km for 16m² and a track range of 45 km for an aircraft with an RCS of 16m² with a LDSD detection range of 6-12 km for 16m² and a LDSD track range of 5-10 km for an aircraft with an RCS of 16m² with a tracking scan range of 30° in azimuth and -7°/+7° in elevation with a scan sweep in 2 to 5 seconds with max tracking target velocity at over 3700 kph with LDSD ground clutter rejection of 20> dB)


Counter Measures: SPO-2B Sirena-2B Generation 0 analogue electronic RWR with 1 target tracked with a single receiver enabling a self protection envelope of 180° in azimuth and ±20° in elevation with band coverage of 6-20 GHz. SSP analogue fire warning system. KKO-3 analogue electronic ECLSS. KS-4 ejection seat. SO-57/SRZO-2 1st Generation analogue electronic IFF interrogator/transponder linked to the Kremnij-2 unsecured analogue IFF system with aircraft ID.


(T models adds SPO-10 Sirena-3M 1st Generation solid state RWR with 4 targets tracked with 4× receivers enabling a self protection envelope of 360° in azimuth and ±90° in elevation with band coverage of 6-20 GHz. SSP-1 analogue fire countermeasure system. SO-63/SRZO-2M 1st Generation solid state IFF interrogator / transponder linked to the Kremnij-2M2 analogue secure IFF system with aircraft ID and basic data encryption. CU32-SORC analogue ICAS and KKO-5LP solid state full ECLSS) 


(1975> TM models add SO-69/SRZO-1P 2nd Generation solid state IFF interrogator / transponder linked to the Parol digital IFF system with aircraft ID, digital data encryption reprogramming and cryptographic encoding)


Electronic Warfare: N/A


Guns: N/A


(T model adds 2× UPK-23-250 23mm twin barrel autocannon pods linked to the ballistic computer with effective firing range up to 2 km)


Ordinance Capacity: 4× hardpoints with a max 2000 kg capacity. 


Common Air to Air Payloads 

2x R-8R 2× R-8T


R-8T

1st Generation IR Missile 

TGS-1 analogue electronic PIR channel Spin Scan PbTe Seeker

~18 km max Range at altitude 

~10 km max Range at sea level 

~8 km engagement range 

~Rear aspect lock range 4 km

~Mach 2 at 5 km+ altitude 

~Mach 1 at sea level 

~Rectile Speed: 50 Hz

~Gimbal limit: 20°

~Angular Tracking: 10 deg/s 

~Turn Rate 4 to 8 Deg/s

~Initial Acceleration of 100-200 m/s>

~Launch limiter 4g 

~Target limiter 4g 

~Overload Tolerance 14g


R-8R

2nd Generation Radar Missile 

PARG-1VV Conical Scanning J band Semi Active Seeker with an analogue electronic parabolic cassegrain antenna array utilising a liquid fuel rocket motor with a radio proximity fuse with a continuous rod warhead enabling a blast radius of 6-10 m²

~30 km max Range at 10 km+ altitude 

~25 km max Range at 5 km+ altitude 

~15 km max Range at sea level 

~8 km engagement range vs RCS of 10m² at sea level 

~20 km engagement range vs RCS of 10m² at 5 km+ altitude 

~22 km engagement range vs RCS of 10m² at 10 km+ altitude 

~1 km NEZ range vs RCS of 10m² at sea level 

~2 km NEZ range vs RCS of 10m² at 5 km> altitude

~3 km NEZ range vs RCS of 10m² at 10 km> altitude

~Mach 2 at 5 km+ altitude 

~Mach 1 at sea level 

~Targeting Angles 20°

~Turn Rate 4 to 8 Deg/s

~Initial Acceleration of 100-200 m/s>

~Launch limiter 4g 

~Target limiter 4g 

~Overload Tolerance 14g



T model adds 


UPK-23-250

AM-23 23×115mm HEI-T

AM-23 23×115mm API-T


R-98T

2nd Generation IR Missile 

TGS-14T LN² Cooled solid state PIR channel Conical Scanning PbS Seeker

~30 km max Range at altitude 

~10 km max Range at sea level

~20 km engagement range 

~Side aspect lock range 2 km

~Rear aspect lock range 8 km

~Mach 2 at 5 km+ altitude 

~Mach 1 at sea level 

~Rectile Speed: 70 Hz

~Gimbal limit: 20°

~Flare Resistance 0.2

~Angular Tracking: 20 deg/s 

~Turn Rate 4 to 8 Deg/s

~Initial Acceleration of 100-200 m/s>

~Launch limiter 4g 

~Target limiter 4g 

~Overload Tolerance 14g


R-98R

3rd Generation Radar Missile 

PARG-14VV Inverse Monopulse J band Semi Active Seeker with a solid state long chord twist cassegrain antenna array with polarisation filtering ECCM utilising a solid fuel rocket motor with a radio proximity fuse with a continuous rod warhead enabling a blast radius of 6-10 m²

~50 km max Range at 10 km+ altitude 

~40 km max Range at 5 km+ altitude 

~20 km max Range at sea level 

~10 km engagement range vs RCS of 5m² at sea level 

~30 km engagement range vs RCS of 5m² at 5 km+ altitude 

~35 km engagement range vs RCS of 5m² at 10 km+ altitude 

~1 km NEZ range vs RCS of 5m² at sea level 

~2 km NEZ range vs RCS of 5m² at 5 km> altitude

~3 km NEZ range vs RCS of 5m² at 10 km> altitude

~Mach 2 at 5 km+ altitude 

~Mach 1 at sea level 

~Targeting Angles 20°

~Turn Rate 4 to 8 Deg/s

~Initial Acceleration of 100-200 m/s>

~Launch limiter 4g 

~Target limiter 4g 

~Overload Tolerance 14g


TM model adds 


Common Air to Air Payloads 

2× R-98MR 2× R-98MT/R-60


R-98MT

2nd Generation IR Missile 

TGS-14T2 LN² Cooled solid state PIR channel Conical Scanning PbS Seeker

~40 km max Range at altitude 

~10 km max Range at sea level

~26 km engagement range 

~Side aspect lock range 2 km

~Rear aspect lock range 8 km

~Mach 2 at 5 km+ altitude 

~Mach 1 at sea level 

~Rectile Speed: 70 Hz

~Gimbal limit: 20°

~Angular Tracking: 20 deg/s 

~Turn Rate 4 to 8 Deg/s

~Initial Acceleration of 100-200 m/s>

~Flare Resistance 0.2

~Launch limiter 4g 

~Target limiter 4g 

~Overload Tolerance 14g


R-98MR

3rd Generation Radar Missile 

PARG-14MVV Inverse Monopulse J band Semi Active Seeker with a solid state long chord twist cassegrain antenna array with polarisation filtering ECCM utilising a solid fuel rocket motor with a radio proximity fuse with a continuous rod warhead enabling a blast radius of 6-10 m²

~50 km max Range at 10 km+ altitude 

~40 km max range at 5 km+ altitude 

~20 km max Range at sea level 

~12 km engagement range vs RCS of 5m² at sea level 

~35 km engagement range vs RCS of 5m² at 5 km+ altitude 

~40 km engagement range vs RCS of 5m² at 10 km+ altitude 

~1 km NEZ range vs RCS of 5m² at sea level 

~3 km NEZ range vs RCS of 5m² at 5 km> altitude

~5 km NEZ range vs RCS of 5m² at 10 km> altitude

~Mach 2 at high altitude 

~Mach 1 at sea level 

~Targeting Angles 20°

~Turn Rate 4 to 8 Deg/s

~Initial Acceleration of 100-200 m/s>

~Launch limiter 4g 

~Target limiter 4g 

~Overload Tolerance 14g


R-60

2nd Generation IR Missile 

OGS-60TI Komar solid state MWIR channel Conical Scanning PbSe Seeker

~12 km max Range 

~12 km max Range at sea level 

~8 km engagement range 

~Side aspect lock range 1 km

~Rear aspect lock range 5 km

~Mach 3 at 5 km+ altitude 

~Mach 2 at sea level 

~Rectile Speed: 100 Hz

~Flare Resistance 0.2

~Gimbal limit: 12°

~Angular Tracking: 35 deg/s 

~Turn Rate 60 to 90 Deg/s

~Initial Acceleration of 300-400 m/s>

~Launch limiter 8g 

~Target limiter 12g 

~Overload Tolerance 42g 



Su-15


Su-15T


Su-15TM 


MiG-19P

Designed: 1951

Prototype: 1954

Production: 1955

Service: 1955

Aircraft Role: Dogfighter 

Generation: 2nd

Number Made: 1000+

Combat Rank: S

Similar Aircraft: F-101


Engine and Airframe: RCS minimum of 5m². 2×  RD-9B turbojets with 52 kN of thrust and 64 kN in afterburner. Top Speed of mach 1.4 at high altitude and mach 0.8 at sea level. Service Ceiling up to 17 km. Combat range of 500-800 km. 


Manuvarabilities: Sustained turn rate of 11-15 deg/s with an instantaneous turn rate of 19-22 deg/s. Roll rate of 100-160 deg/s. Climb rate of 170-190 m/s. Overload tolerance of 5-8g. Angle of attack 18-20°. 


Avionics: Hydromechanical AFCS. RP-1 Izumrud J band 1st Generation air interception radar. ARK-5P analogue ADF. 1st Generation cockpit. RSIU-3 analogue radio. Gorizont-1 data link with automated GCI. SVS-16 9 pin Nuvistor FCC. 


Targeting Systems: RP-1 Izumrud 1st Generation air interception radar with a horizontal scan range of 30° and a vertical scan range of -7°/+7° with a max detection range up to 12 km with a track range of 2 km for an aircraft with an RCS of 10m². ASP-5N 1st Generation HUD. 1st Generation Radar display with a CRT screen utilising a raw signal oscillator for target engagement. 


(Early models used SRD-1 Rangefinding Radar and ASP-5N HUD only) 


(Later models added RP-5 Sokol 1st gen radar with improved track range of 4 km) 


Countermeasures: SPO-2B Sirena-2B 1st Generation RWR. KK-2 ejection seat. SSP-2I fire warning system. 


Guns: 3× NR-30 30mm autocannon slaved to radar with an effective firing range up to 1 km. 


Ordinance Capacity: 2× hardpoints with a 500 kg munition capacity and 205 rounds for guns. 


Common Air to Air Payloads 

2×7 ORO-57 Proximity fuse Rocket Pods 

2× RS-1U 


ORO-57

S-5 KEP

S-5M HE-FRAG

S-5S Flechette 


RS-1U

1st Gen Radar Missile 

K-5 Beam Riding Seeker

~6 km Range 

~Mach 2 speed 


Later models add 


Common Air to Air Payloads 

2× R-3T

2× R-5



Later models add 



Sources on SMR main document under equipment details 


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