| Manufacturer | Grumman |
| Model | F10F Jaguar |
| Modification | F10F-1 |
| Country | USA |
| Years | 1952 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | - |
| Length | 16.52 m |
| Height | 4.95 m |
| Wing area | 41.81 m2 |
| Zero fuel weight | - |
| Empty weight | 9265 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 16080 kg |
| Flight duration | - |
| Engine | 1 ТРД Westinghouse XJ40-WE-8 |
| Power | - |
| Thrust | 1 x 48.50 kN |
| Maximum speed | 1143 km/h |
| Cruising speed | 1017 km/h |
| Rate of climb | - |
| Practical range | 2687 km |
| Service ceiling | 13960 m |
| Hovering ceiling | - |
| Crew | 1 |
