| 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 |