Chengdu J-10 Firebird (Jian-10 Fighter aircraft 10) / F-10
| Specifications | ||
|---|---|---|
| Model | J-10 | J-10U carrier type | 
| Wing Span | 8.78m | 8.78 meters | 
| Length | 14.57m | 14.57 meters | 
| Height | 4.78m | 5.3 meters | 
| sweep angle | 50-52 degrees, | |
| wing area | 38 square meters | |
| vertical tail area | 8.4 square meters | |
| Empty weight | 8,840 kg | |
| Weight | 9,750kg | |
| Takeoff weight | 18,600 kg | 18270 kg | 
| maximum external fuel tank | 4100 liters (1500 × 2, 1100 × 1) | |
| Engine | 1 | |
| Engine | Saturn AL-31FN afterburning turbofan | |
| thrust | 122 kilonewtons | 152 kilonewtons | 
| thrust-to-weight ratio | greater than 1.1 | |
| Maximum speed | M1.85 / 2,700 kilometers per hour | |
| Maximum speed at high altitude | Mach 2.0 | |
| Maximum speed at low altitude | Mach 1.2 (1473 km / h) | |
| Cruising speed | ||
| Range | 3,900 km | 3000 kilometers | 
| Combat radius | 1300 kilometers | |
| Service Ceiling | 18,000m | 18,000 meters | 
| Takeoff and landing distance | less than 50 meters | |
| Armament | ... | 6000 kg ammunition load | 
| Crew | 1 or 2 | 1 or 2 | 
| Cost | . . | |
| 
NEWSLETTER
 | 
| Join the GlobalSecurity.org mailing list | 
|  |  | 

