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The Tupolev Tu-75 (Russian: Туполев Ту-75) was a military transport variant of the Tu-4 bomber, as was a similar airliner, the Tu-70, both using a new, purpose-designed fuselage. The first Soviet military machine of this class, it was equipped with a rear fuselage loading ramp. It was not placed into production because the VVS decided it would be cheaper to modify its existing Tu-4s for the transport mission and to use its existing Lisunov Li-2 and Ilyushin Il-12 transports.

Tu-75
Role transport
National origin Soviet Union
Manufacturer Tupolev
First flight 21 January 1950
Status Cancelled
Number built 1

Design and development


The Tupolev OKB began work in September 1946 on a military transport version of the Tupolev Tu-70 airliner and this was confirmed by the Council of Ministers on 11 March 1947 with state trials to begin in August 1948. To expedite the process, maximum use was made of components of the Tu-70. Its engines were the uprated Shvetsov ASh-73TKFN or TKNV fuel-injected version. A new, narrower fuselage was designed, which included a rear cargo hatch, a vehicle loading ramp and paratroop exit doors. Three gun turrets (dorsal, ventral and tail), were to be adapted from the Tu-4, although they were not fitted on the prototype. It had a crew of six (two pilots, three gunners, a radio operator, and a navigator).[1]

The aircraft was intended for three different roles; transport, parachute transport and aerial ambulance. In the first role it was designed to carry two ASU-76 assault guns, two STZ NATI artillery tractors, six or seven GAZ-67B jeeps or five 85 mm (3.3 in) guns without their prime movers or any combination of equipment up to 12,000 kg (26,000 lb). To facilitate the loading of cargo, a winch was mounted on the ceiling of the cargo hold with a capacity of 3,000 kg (6,600 lb). It could carry either 120 troops, 96 fully loaded paratroopers or 64 standard parachute loads. As an aerial ambulance it could carry 31 stretchers and four medical attendants.[2]


Operational history


Construction of the first prototype was quite prolonged; the aircraft was not finished until November 1949, with its first flight taking place on 21 January 1950. It finished its manufacturer's trials the following May, but Tupolev decided not to submit it for the State acceptance trials as the Soviet Air Force had already decided that it would be cheaper to rely on its existing transports and to modify Tu-4 bombers for the cargo role. The prototype was used by the MAP (Russian: Ministerstvo Aviatsionnoy Promyshlennosti – Ministry of Aviation Industry) until it crashed in October 1954.[3]


Specifications


Data from The Osprey Encyclopedia of Russian Aircraft 1875-1995[4]

General characteristics

Performance

Armament


See also


Related development

Aircraft of comparable role, configuration, and era


References



Notes


  1. Gordon and Rigamant, p. 107
  2. Gordon and Rigamant, p. 108
  3. Gordon and Rigamant, p. 109
  4. Gunston 1995

Bibliography



На других языках


[de] Tupolew Tu-75

Die Tupolew Tu-75 (russisch Туполев Ту-75, NATO-Codename: „Cart“) ist ein vom sowjetischen Konstruktionsbüro Tupolew entwickeltes militärisches Transportflugzeug aus den 1950er-Jahren. Sie wurde aus der Tupolew Tu-70 entwickelt, die wiederum auf dem Tupolew Tu-4-Bomber basierte, jedoch einen neu entwickelten Rumpf besaß und speziell für Transportaufgaben entwickelt wurde.
- [en] Tupolev Tu-75

[fr] Tupolev Tu-75

Le Tupolev Tu-75 est la version de transport militaire du bombardier Tupolev Tu-4.

[it] Tupolev Tu-75

Il Tupolev Tu-75 (in caratteri cirillici Туполев Ту-75) era un quadrimotore da trasporto tattico ad ala bassa progettato dall'OKB 156 diretto da Andrej Nikolaevič Tupolev e sviluppato in Unione Sovietica nella seconda parte degli anni quaranta.

[ru] Ту-75

Ту-75 — советский военно-транспортный самолёт, спроектирован на базе пассажирского Ту-70 (пассажирский вариант бомбардировщика Ту-4). В соответствии с техническим заданием это должен быть четырёхмоторный средний транспортный самолёт с максимальной коммерческой нагрузкой 12-13 т, дальностью 2500 км. Максимальная скорость на высоте 5000 м — 500 км/ч, потолок — 9000 м, скороподъёмностью — 20 минут до высоты 5000 м. Самолёт должен иметь оборонительное вооружение.[1]



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