Manufacturer | Atlas |
Model | Cheetah |
Modification | Cheetah С |
Country | South Africa |
Years | 1986 |
Type | Fighter |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 8.22 m |
Length | 15.55 m |
Height | 4.50 m |
Wing area | 34.80 m2 |
Zero fuel weight | - |
Empty weight | 6600 kg |
Maximum takeoff weight | 13700 kg |
Normal takeoff weight | - |
Flight duration | - |
Engine | 1 ТРД SNECMA Atar 9K50C-11 |
Power | - |
Thrust | 1 x 71 kN |
Maximum speed | - |
Cruising speed | - |
Rate of climb | 14000 m/min |
Practical range | 1300 km |
Service ceiling | 17000 m |
Hovering ceiling | - |
Crew | 1 |