| serial | Tu-110A 4AL-7P
|
| First flight | March 11, 1957
|
| Total built | 3
|
| Manufacturer | Union of Soviet Socialist Republics
|
| Design | KB Tupolev
|
| length of the aircraft | 40.06 m;
|
| wing span | 36.98 m;
|
| height of the aircraft | 11.53 m;
|
| area of the wing | 186.115 m²
|
| Max. takeoff weight | 82700 kg;
|
| Engines | 4 TRD AL-7P
|
| Thrust (power) | 4 x 6700
|
| Maximum speed | 878 km / h
|
| Cruising speed | 750-800 km / h;
|
| maximum range flight | 3500-4500 km;
|
| practical ceiling | 12000 m;
|
| number of passengers | 100 people;
|
| crew | 5 people
|
| VARIANTS |
|
|---|
| Tu-110 | The only prototype of the Tu-110 (CCCP-5600).
|
| Tu-110A | Model with an increased maximum take-off weight of 87 200 kg. Three aircraft were built (CCCP-5511).
|
| Tu-110B | Model with four turbojet engines D-20 .
|
| 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.
|
| Tu-117 | Remained in the draft military transport version with a defensive tower in the rear of the fuselage.
|
