Manufacturer | McDonnell Douglas |
Model | A-4F Skyhawk |
Modification | А-4F |
Country | USA |
Years | 1966 |
Type | Attack aircraft |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 8.38 m |
Length | 12.29 m |
Height | 4.57 m |
Wing area | 24.16 m2 |
Zero fuel weight | - |
Empty weight | 4809 kg |
Maximum takeoff weight | - |
Normal takeoff weight | 11113 kg |
Flight duration | - |
Engine | 1 ТРД Pratt Whitney J52-P-8А |
Power | - |
Thrust | 1 x 4218 kN |
Maximum speed | 1078 km/h |
Cruising speed | 1024 km/h |
Rate of climb | - |
Practical range | 3800 km |
Service ceiling | 12880 m |
Hovering ceiling | - |
Crew | 1 |