Armament
* Guns:
1× mounted 23 mm twin-barrel GSh-23 cannon with 220 rounds of ammunition.
* Hardpoints:
8 total: 1× beneath the port-side intake trunk, 6× under-wing, and 1× under-fuselage with a capacity of 4000 kg external fuel and ordnance,
* Missiles:
* Air-to-air missiles:
- Vympel R-77 (NATO reporting name: AA-12 Adder)
- Vympel R-73 (NATO reporting name: AA-11 Archer)
* Air-to-surface missiles:
- Kh-59ME TV guided standoff Missile / Laser guided standoff Missile
* Anti-ship missile
* Bombs:
* KAB-1500L laser guided bombs
* FAB-500T dumb bombs
* OFAB-250-270 dumb bombs
* OFAB-100-120 dumb bombs
* RBK-500 cluster bombs
Place of origin India
Manufacturer DRDO
Produced May 9, 2003
Specifications
Weight 154 kg
Length 3570 mm
Diameter 178 mm
Warhead 15 kg (33 lb) HE fragmentation directional warhead
Detonation
mechanism Radar proximity fuze
Engine Solid Fuel Rocket
Wingspan 254 mm
Operational
range 80 km head on, 15 km tail chase
Flight ceiling 66,000 ft
Speed Mach 4 +
Guidance
system Inertial, mid-course update and terminal active radar homing (15 km)
Place of origin Russia
Manufacturer Vympel
Produced 1994
Specifications
Weight 175 kg (R-77), 226 kg (R-77M1)
Length 3.6 m (R-77)
Diameter 200 mm
Warhead 30 kg HE, fragmenting
Detonation
mechanism laser proximity fuze
Engine Solid fuel rocket motor (R-77), air-breathing ramjet (R-77M1)
Wingspan 350 mm
Operational
range R-77: 90 km (55.92MI)
R-77M1: 175 km (108.7MI)
Flight altitude 5m-25 km (16.5-82,000 ft)
Speed Mach 4 (R-77)
Guidance
system Inertial with mid-course update and terminal active radar homing
Place of origin Russia
Manufacturer Vympel
Produced 1985
Specifications
Weight 105 kg (231 lb)
Length 2900 mm (9 ft 6 in)
Diameter 170 mm (6.7 in)
Warhead 7.4 kg (16.3 lb)
Engine solid-fuel rocket engine
Wingspan 510 mm (20 in)
Operational
range 30 km (18.75 mi)
Speed Mach 2.5
Guidance
system infrared homing
Place of origin Russia
Manufacturer Raduga
Produced 1991
Specifications
Weight 930 kg (2,050 lb)
Length 570 cm (220 in)
Diameter 38.0 cm (15.0 in)
Warhead Cluster or shaped-charge fragmentation
Warhead weight 320 kg (705 lb)
Engine Kh-59 :two-stage rocket
Kh-59ME :rocket then turbofan
Wingspan 130 cm (51.2 in)
Operational
range Kh-59ME(export) :115 km (62 nmi)
Kh-59ME : 200 km (110 nmi)
Kh-59MK : 285 km (150 nmi)
Speed Mach 0.72-0.88
Guidance
system inertial, then TV-guided
