Attribute | Value |
---|---|
General | |
Manufacturer | Grumman |
Model | Grumman OV-1 Mohawk |
Country | United States |
Manufactured from | 1959 year |
Manufactured to | 1970 year |
Type | Military Propellor Planes |
Icao | OV1 |
Performance | |
Engine | 2x Lycoming T53-L-701 |
Power, hp | 1,400 hp |
Power, lbf | Add |
Avionics | Add |
Max cruise speed | 491 km/h |
Approach speed | 135 km/h |
Travel range | 1,519 km |
Fuel economy | Add |
Service ceiling | 7,620 m |
Rate of climb | 17.78 m/sec |
Take off distance | 358 m |
Landing distance | 320 m |
Weights | |
Max take off weight | 8,215 kg |
Max landing weight | 7,051 kg |
Max payload | 1,050 kg |
Fuel tank capacity | 1,045 l |
Baggage volume | Add |
Dimensions | |
Seats | 2 |
Seats - business class | Add |
Seats - first class | Add |
Cabin height | Add |
Cabin width | Add |
Cabin length | Add |
Exterior length | 12.5 m |
Tail height | 3.86 m |
Fuselage diameter | 1.7 m |
Wing span | 14.63 m |
Wing tips | No Winglets |