Chengdu J-10
Fighter / Fighter Bomber
The Chengdu J-10 is a single-engine single-seat multi-role combat aircraft produced by the Chinese manufacturer Chengdu Aircraft Industry Corporation.
Propulsion | 1 Turbofan Engine |
Engine Model | Saturn AL-31FN |
Engine Power dry/with Afterburner | 86,0 / 123,0 kN | 19334 / 27652 lbf |
Speed | 2450 km/h | 1323 kts 1522 mph |
Mmo (max. Mach) | Mach 1.85 |
Service Ceiling | 18.000 m | 59.055 ft |
Range | 1.852 km | 1.000 NM 1.151 mi. |
Empty Weight | 6.940 kg | 15.300 lbs |
max. Takeoff Weight | 18.400 kg | 40.565 lbs |
Wing Span | 8,78 m | 28 ft 10 in |
Wing Area | 33,1 m² | 356 ft² |
Length | 14,57 m | 47 ft 10 in |
Height | 4,80 m | 15 ft 9 in |
First Flight | 24.03.1998 |
Production Status | in production |
ICAO Code | J10 |
Data for (Version) | Chengdu J-10 |
Variants | J-10A, J-10S |