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 |
