General characteristics

• Crew: 1

• Length: 19.8 m (65.0 ft)

• Wingspan: 13.95 m (45.8 ft)

• Height: 4.74 m (15.6 ft)

• Wing area: 78.8 m2 (848.1 ft2)

• Empty weight: 18,000 kg (39,680 lb)

• Loaded weight: 25,000 kg (55,115 lb) typical mission weight, 29,270 kg (64,530 lb) at full load

• Max. takeoff weight: 35,000 kg (77,160 lb)

• Powerplant: 2 × izdeliye 30 thrust vectoring turbofan

  • Dry thrust: 93.1 kN / 107 kN (21,000 lbf / 24,300 lbf) each

  • Thrust with afterburner: 147 kN / 167 kN (33,067 lbf / 37,500 lbf) each

• Fuel capacity: 10,300 kg (22,700 lb)

Performance

• Maximum speed:

  • At altitude: Mach 2.3 (2,440 km/h, 1,520 mph)

  • Supercruise: Mach 1.6 (1,700 km/h, 1,060 mph)

• Range: 3,500 km (2,175 mi) subsonic

  • 1,500 km (930 mi) supersonic

• Ferry range: 5,500 km (3,420 mi) with one in-flight refueling

• Service ceiling: 20,000 m (65,000 ft)

• Wing loading: 317–444 kg/m2 (65–91 lb/ft2)

• Thrust/weight:

  • 1.16 (1.36 at typical mission weight)

• Maximum g-load: +9.0 g

Armament

• Guns: 1× 30 mm (1.181 in) 9A1-4071K (GSh-301) cannon in right LEVCON root

• Air to air loadout:

  • 4× K-77M or 4× izdeliye 810

  • 2× K-74M2 or 2× izdeliye 300

• Air to ground loadout:

  • 4× Kh-38M or 4× Kh-58UShK or 8× KAB-250 or 4× KAB-500

  • 2× K-74M2 or 2× izdeliye 300

• Air to sea loadout:

  • 4× Kh-35

  • 2× K-74M2 or 2× izdeliye 300

• Hardpoints: Six external hardpoints.

  • Kh-31

  • R-73

  • R-77

Avionics

• Sh121 multifunctional integrated radio electronic system (MIRES)

  • N036 Byelka radar system

    • N036-1-01: Frontal X-band AESA radar

    • N036B-1-01: Cheek X-band AESA radars for increased angular coverage

    • N036L-1-01: Slat L-band arrays for IFF

  • L402 Himalayas Electronic countermeasure suite

• 101KS Atoll electro-optical system

  • 101KS-O: Laser Directional Infrared Counter Measures

  • 101KS-V: Infra-red search and track

  • 101KS-U: Ultraviolet Missile Approach Warning system

  • 101KS-N: Targeting pod