Attribute | Value |
---|---|
General | |
Manufacturer | Tupolev |
Model | Tupolev Tu-95 |
Country | Russia |
Manufactured from | 1956 year |
Manufactured to | 1993 year |
Type | Military Propellor Planes |
Icao | TU95 |
Performance | |
Engine | 4x 4 × Kuznetsov NK-12MV turboprops |
Power, hp | 15,000 hp |
Power, lbf | Add |
Avionics | Add |
Max cruise speed | 815 km/h |
Approach speed | Add |
Travel range | 15,001 km |
Fuel economy | 0.323 km/l |
Service ceiling | 13,716 m |
Rate of climb | 10.16 m/sec |
Take off distance | Add |
Landing distance | Add |
Weights | |
Max take off weight | 188,000 kg |
Max landing weight | Add |
Max payload | 5,000 kg |
Fuel tank capacity | 110,155 l |
Baggage volume | Add |
Dimensions | |
Seats | 7 |
Seats - business class | Add |
Seats - first class | Add |
Cabin height | Add |
Cabin width | Add |
Cabin length | Add |
Exterior length | 49.1 m |
Tail height | 13.4 m |
Fuselage diameter | 2.9 m |
Wing span | 50.1 m |
Wing tips | No Winglets |