| Technical data | |
|---|---|
| Type | Tu-91 |
| Function | attack |
| Year | 1955 |
| Crew | 2 |
| Engines | 1*7650hp TV-2M |
| Wing Span | 16.4m |
| Length | 17.7m |
| Height | 5.06m |
| Wing Area | 47.48m2 |
| Empty Weight | 12850kg |
| Maximum Weight | 14400kg |
| Speed | 800km/h |
| Ceiling | 11000m |
| Range | 2350km |
| Armament | |
| Bombs/Rockets | 1500kg |
Naval attack bomber. The operational need for the Tu-91 disappeared after Stalin's death, when the ship-building programme was cut back and the carriers cancelled. Moreover, there were more pure political troubles. There was a competing Ilyushin's project, and Ilyushin's team was considered to be more skilled in this class of aircraft.
Another trouble was that Tu-91 was demonstrated to N.S.Khruschew with rocket armament option, despite it was known that Nikita Sergeevich always was skeptical about efficiency of air-surface rockets... (Damn it, what CPSU leader personal scepticism has to do with such a choice? Is he a military expert of any sort?)
The Tu-91 had a powerful turboprop in the mid fuselage, behind the cockpit, with split exhausts behind the wing roots, driving a big three-bladed contra-rotating propeller. It had straight wings, but slightly swept tail plane and fin.
| Modified February 25, 1996 |
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