Attribute | Value |
---|---|
General | |
Manufacturer | MIL Helicopters |
Model | Mil Mi-8 “Hip” |
Country | Russia |
Manufactured from | 1961 year |
Manufactured to | Add |
Type | Military Helicopters |
Icao | Add |
Performance | |
Engine | 2 × Klimov TV3-117Mt turboshafts - |
Power, hp | 1,950 hp |
Power, lbf | Add |
Avionics | Add |
Max cruise speed | 224 km/h |
Approach speed | Add |
Travel range | 959 km |
Fuel economy | 0.298 km/l |
Service ceiling | 4,500 m |
Rate of climb | 8.99 m/sec |
Take off distance | Add |
Landing distance | Add |
Weights | |
Max take off weight | 12,000 kg |
Max landing weight | Add |
Max payload | 3,000 kg |
Fuel tank capacity | 3,702 l |
Baggage volume | Add |
Dimensions | |
Seats | 28 |
Seats - business class | Add |
Seats - first class | Add |
Cabin height | 1.26 m |
Cabin width | 1.2 m |
Cabin length | Add |
Exterior length | 18.17 m |
Tail height | Add |
Fuselage diameter | Add |
Wing span | 21.29 m |
Wing tips | No Winglets |