General characteristics
- Crew: 1
- Length: 21.9
m (72.9 ft)
-
Wingspan: 15.3
m (50.2 ft, with wingtip pods)
- Height: 5.90
m (19.4 ft)
- Wing area: 62.0
m² (667 ft²)
-
Empty weight: 18,400
kg (40,570 lb)
- Loaded weight: 25,300
kg (56,660 lb) at 50% internal fuel
-
Max. takeoff weight: 34,500
kg (76,060 lb)
-
Powerplant: 2
× Saturn
117S (AL-41F1S) afterburning turbofan with
3D thrust
vectoring nozzle
- Dry thrust: 8,800
kgf (86.3 kN, 19,400 lbf) each
- Thrust with afterburner: 14,500
kgf (142 kN, 31,900 lbf) each
- Fuel capacity: 11,500 kg
(25,400 lb) internally
Performance
-
Maximum speed:
- At altitude: Mach
2.25 (2,390 km/h, 1,490 mph)
- At sea level: Mach
1.15 (1,400 km/h, 870 mph)
-
Range:
- At altitude: 3,600
km (1,940 nmi)
- At sea level: 1,580
km (850 nmi)
-
Ferry range: 4,500
km (2,430 nmi) with 2 external fuel tanks
-
Service ceiling: 18,000
m (59,100 ft)
-
Rate of climb: >280
m/s (>55,000 ft/min)
-
Wing loading: 408
kg/m² (500.8 kg/m² with full internal fuel) (84.9 lb/ft² 50%
fuel)
-
Thrust/weight: 1.13
at 50% fuel (0.92 with full internal fuel)
- Maximum g-load: +9 g
Armament
- Guns: 1×
30 mm GSh-301 internal
cannon with 150 rounds
-
Hardpoints: 12
hardpoints, consisting of 2 wingtip rails, and 10 wing and
fuselage stations with a capacity of 8,000 kg (17,630 lb) of ordnance and
provisions to carry combinations of:
- Rockets:
-
S-25L laser-guided
rocket
-
S-25 unguided
rocket
-
B-8 unguided
S-8 rocket pods
-
B-13 unguided
S-13 rocket pods
- Missiles:
- Bombs:
- FAB-250 250-kilogram
(550 lb) unguided bombs
- FAB-500 500-kilogram
(1,100 lb) unguided bombs
-
KAB-500L laser-guided
bomb
- KAB-1500 laser-guided
bomb
- Other:
Avionics
wikipedia.org
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