Tupolew / Tupolev Tu-95
Long-Range Bomber
The Tupolev Tu-95 is a four-engine strategic bomber developed by the Soviet Design Bureau OKB Tupolev.
A further development of the Tu-95 for maritime reconnaissance / anti-submarine warfare the Tu-142.
| Propulsion | 4 Turboprop Engines |
| Engine Model | Kuznetsov NK-12M |
| Engine Power (each) | 10889 kW | 14602 shp |
| Speed | 830 km/h | 448 kts
516 mph |
| Service Ceiling | 12.000 m | 39.370 ft |
| Range | 14.999 km | 8.099 NM
9.320 mi. |
| Empty Weight | 81.670 kg | 180.051 lbs |
| max. Takeoff Weight | 167.880 kg | 370.112 lbs |
| Wing Span | 50,04 m | 164 ft 2 in |
| Wing Area | 310,5 m² | 3342 ft² |
| Length | 49,13 m | 161 ft 2 in |
| Height | 13,20 m | 43 ft 4 in |
| First Flight | 12.11.1952 |
| Production Status | out of production |
| Total Production | >300 |
| ICAO Code | TU95 |
| NATO Code | Bear |
| Data for (Version) | Tupolev / Tupolew Tu-95MS |
