Projected)
Most of these figures are for the Sukhoi T-50 prototype and not the finished HAL FGFA.
Data from HAL
General characteristics
- Crew: 1 (pilot)
- Length: 22.6 m
- Wingspan: 14.2 m (46 ft 7 in)
- Height: 5.9 m
- Wing area: 78.8 m² (848 ft²)
- Empty weight: 18,500 kg (40,786 lb)
- Loaded weight: 26,000 kg (57,320 lb)
- Useful load: 7,500 kg (16,535 lb)
- Max. takeoff weight: 34,000 kg
- Powerplant: 2 × Saturn-Lyulka AL-41F turbofans
- Dry thrust: 96.1 kN (9,800 kgf, 21,605 lbf) each
- Thrust with afterburner: 152 kN (15,500 kgf, 34,172 lbf) each
Performance
- Maximum speed: 2,100 - 2,500 km/h (Mach 2+) (1,305 mph+)
- g-limits: (10-11 g)
- Cruise speed: 1,850 - 2,100 km/h (1,150 - 1,300 mph)
- Combat radius: 1,500 km
- Ferry range: 5,500 km (3,400 mi)
- Service ceiling: 20,000 m (65,617 ft)
- Rate of climb: 350 m/s (68,898 ft/min)
- Wing loading: 330 (normal) - 470 (maximum) kg/m2 (67 (normal) - 96 (maximum) lb/ft2)
- Thrust/weight: 1.19
- Runway: 350 m (1,148 ft)
- Endurance: 3.3 hrs (198 mins)
Armament
- Guns: 2× 30 mm internal cannon
- Hardpoints: 16 total, 8 internal, 8 on wings.
Avionics
- Radar: N050 BRLS AESA/PESA Radar (Enhancement of IRBIS-E) on SU-35
- Frequency: X (8 - 12 GHz)
- Diameter: 0.7 m (2 ft 4 in)
- Targets: 32 tracked, 8 engaged
- Range: > 400 km (248 mi)
- EPR: 3 m² (32.3 ft²) at 400 km (248 mi)
- RCS: 3 m ² to 400 km, 1 m ² to 300 km, 0.5 m ² to 240 km, 0.1m ² to 165 km, 0.01M ² to 90 km.
- Azimuth: 240 ° (± 120 °)
- Power: 5,000 W
- Weight: 65 to 80 kg (143 to 176 lb)
Read more about this topic: Sukhoi/HAL FGFA, Specifications (PAK FA and FGFA