Comparison of Tupolev Tu-114 and Tupolev Tu-95 [S]ave
| Attribute |  Tupolev Tu-114 × |  Tupolev Tu-95 × |
|---|---|---|
| General | ||
| Manufacturer | Tupolev | Tupolev |
| Model | Tupolev Tu-114 | Tupolev Tu-95 |
| Country | Russia | Russia |
| Manufactured from (year) | 1958 | 1956 |
| Manufactured to (year) | 1963 | 1993 |
| Type | Passenger Turbo Props | Military Propellor Planes |
| Icao | TU114 | TU95 |
| Performance | ||
| Engine | 4x Kuznetsov NK-12MV | 4x 4 × Kuznetsov NK-12MV turboprops |
| Power, hp (hp) | 14,795 | 15,000 |
| Max cruise speed (km/h) | 880 | 815 |
| Travel range (km) | 8,945 | 15,001 |
| Fuel economy (km/l) | - | 0.323 |
| Service ceiling (m) | 11,887 | 13,716 |
| Rate of climb (m/sec) | 10.16 | 10.16 |
| Take off distance (m) | 2,500 | - |
| Landing distance (m) | 1,400 | - |
| Weights | ||
| Max take off weight (kg) | 171,000 | 188,000 |
| Max payload (kg) | 20,000 | 5,000 |
| Fuel tank capacity (l) | 72,983 | 110,155 |
| Dimensions | ||
| Seats | 23 | 7 |
| Exterior length (m) | 54.1 | 49.1 |
| Tail height (m) | 15.44 | 13.4 |
| Fuselage diameter (m) | 3.3 | 2.9 |
| Wing span (m) | 51.1 | 50.1 |
| Wing tips | No Winglets | No Winglets |
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