| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Grumman |
| Model | Grumman F11F Tiger |
| Country | United States |
| Manufactured from | 1954 year |
| Manufactured to | 1959 year |
| Type | Fighter Jets |
| Icao | F11F |
| Performance | |
| Engine | 1x Wright J65-W-18 afterburning turbojet |
| Power, hp | Add |
| Power, lbf | 10,500 lbf |
| Avionics | AN/ARC-27A UHF COMMS, AN/ARA-25 UHF, AN/ARR-40 UHF, AN/ARN-14E VHF Nav etc. |
| Max cruise speed | 1,213 km/h |
| Approach speed | Add |
| Travel range | 2,056 km |
| Fuel economy | Add |
| Service ceiling | 12,771 m |
| Rate of climb | 82.8 m/sec |
| Take off distance | Add |
| Landing distance | Add |
| Weights | |
| Max take off weight | 10,641 kg |
| Max landing weight | 9,541 kg |
| Max payload | 1,360 kg |
| Fuel tank capacity | 3,872 l |
| Baggage volume | Add |
| Dimensions | |
| Seats | 1 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | Add |
| Exterior length | 13.98 m |
| Tail height | 4.03 m |
| Fuselage diameter | 0.7 m |
| Wing span | 9.64 m |
| Wing tips | No Winglets |