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 |