Manufacturer | Shenyang |
Model | J-8 |
Modification | J-8 |
Country | China |
Years | 1969 |
Type | Fighter |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 9.34 m |
Length | 21.52 m |
Height | 5.41 m |
Wing area | 42.00 m2 |
Zero fuel weight | - |
Empty weight | 9285 kg |
Maximum takeoff weight | 16580 kg |
Normal takeoff weight | 13700 kg |
Flight duration | - |
Engine | 2 ТРДФ Liyang (LMC) Wopen-7A (Р-11Ф) |
Power | - |
Thrust | - |
Maximum speed | 2332 (M=2.2) km/h |
Cruising speed | 850 km/h |
Rate of climb | - |
Practical range | 1500 km |
Service ceiling | 20800 m |
Hovering ceiling | - |
Crew | - |