serial | Tu-110A 4AL-7P
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First flight | March 11, 1957
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Total built | 3
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Manufacturer | Union of Soviet Socialist Republics
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Design | KB Tupolev
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length of the aircraft | 40.06 m;
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wing span | 36.98 m;
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height of the aircraft | 11.53 m;
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area of the wing | 186.115 m²
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Max. takeoff weight | 82700 kg;
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Engines | 4 TRD AL-7P
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Thrust (power) | 4 x 6700
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Maximum speed | 878 km / h
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Cruising speed | 750-800 km / h;
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maximum range flight | 3500-4500 km;
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practical ceiling | 12000 m;
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number of passengers | 100 people;
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crew | 5 people
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VARIANTS |
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Tu-110 | The only prototype of the Tu-110 (CCCP-5600).
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Tu-110A | Model with an increased maximum take-off weight of 87 200 kg. Three aircraft were built (CCCP-5511).
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Tu-110B | Model with four turbojet engines D-20 .
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Tu-110D | In 1960, the design bureau of Tupolev Design Bureau proposed a long-range Tu-110D aircraft with the arrangement of two-circuit turbojet engines D-20 P designed by PA Soloviev in the tail part of the fuselage. It was expected that the flight range would reach 4,500 - 5,000 km, but the project was not supported in Minaviaprom because of the low resource of the D-20P.
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Tu-117 | Remained in the draft military transport version with a defensive tower in the rear of the fuselage.
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