| 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 |
