| Manufacturer | Grumman |
| Model | F9F Cougar |
| Modification | F9F-6 |
| Country | USA |
| Years | 1951 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 10.52 m |
| Length | 12.47 m |
| Height | 3.73 m |
| Wing area | 27.87 m2 |
| Zero fuel weight | - |
| Empty weight | 5209 kg |
| Maximum takeoff weight | 9526 kg |
| Normal takeoff weight | 8367 kg |
| Flight duration | - |
| Engine | 1 ТРД Pratt Whitney J48-P-8A |
| Power | - |
| Thrust | 1 x 3289 kN |
| Maximum speed | 1135 km/h |
| Cruising speed | 870 km/h |
| Rate of climb | - |
| Practical range | 1500 km |
| Service ceiling | 13715 m |
| Hovering ceiling | - |
| Crew | 1 |
