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Tupolev Tu-104

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Tu-104
250px
Aeroflot Tu-104
Type Airliner
Manufacturer Tupolev OKB
Maiden flight 1955-06-17
Introduced 1956-09-15 with Aeroflot
Retired 1981
Primary users Aeroflot
ČSA
Interflug
Produced 1956-1960
Number built 200

The Tupolev Tu-104 (NATO reporting name: Camel) was a twin-engined medium-range turbojet-powered Soviet airliner. After the British de Havilland Comet and Canadian Avro Jetliner, the Tu-104 was the third jet airliner to fly and the first to enter regular service. Known in the west by its NATO moniker, its arrival in London during a 1956 state visit shocked Western observers.

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[edit] Development

At the beginning of the 1950s, the Soviet Union's Aeroflot airline desperately needed a modern airliner with better capacity and performance than any Soviet plane then in operation. The design request was filled by the Tupolev OKB, which based their new airliner on its Tu-16 'Badger' strategic bomber. The wings, engines, and tail surfaces of the Tu-16 were retained in the airliner, but the new design adopted a wider, pressurised fuselage to accommodate 50 passengers. The first flight of first serial Tu-104 was on November 6, 1955 on Kharkiv plant in Ukraine.

By the time production ceased in 1960, about 200 had been built. Aeroflot did not retire the Tu-104 from civil service until 1981. CSA Czechoslovak Airlines, the Czechoslovak national airline, bought a small number of Tu-104As configured for 81 passengers.

Following its removal from civil service, several disbanded aircraft were transferred to the Soviet military, which used them as staff transports and to train cosmonauts in zero gravity.

[edit] Variants

  • Tu-104 - initial version seating 50 passengers.
  • Tu-104A - Continuing improvements in the Mikulin engines permitted significant growth in the Tu-104 resulting in a 70-seater variant. The Tu-104A became the definitive production variant.
    • Tu-104D - Tu-104A airframes rebuilt to accommodate 85 passengers
    • Tu-104V - Tu-104A airframes rebuilt to accommodate 100 passengers
  • Tu-104B - Further improvements were attained with the stretched Tu-104B fitted with new engines, the Mikulin AM-3M-500 turbojets, and able to accommodate 100 passengers.
  • Tu-104E - Record breaking version.
  • Tu-110 - Four-engined transport prototype.

[edit] Specifications (Tu-104B)

General characteristics<h3>
  • Crew: 7
  • Capacity: 50-100 passengers
  • Length: 40.05 m (131 ft 5 in)
  • Wingspan: 34.54 m (113 ft 4 in)
  • Height: 11.90 m (39 ft 0 in)
  • Wing area: 184 m² (1,975 ft²)
  • Empty weight: 41,600 kg (91,710 lb)
  • Max takeoff weight: 76,000 kg (167,550 lb)
  • Powerplant:Mikulin AM-3M-500 turbojets, 95.1 kN (21,400 lbf) each
<h3>Performance<h3>


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[edit] References and external links

[edit] Related content

Related development<h3> Tu-16 - Tu-107 - Tu-110 - Tu-124

<h3>Comparable aircraft<h3> de Havilland Comet <h3>Designation sequence<h3> Tu-99 - Tu-102 - Tu-103 - Tu-104 - Tu-105 - Tu-106 - Tu-107

de:Tupolew Tu-104

fi:Tupolev Tu-104 he:טופולב Tu-104 ja:Tu-104 (航空機) ru:Ту-104 sv:Tupolev Tu-104 sr:Тупољев Ту-104 uk:Ту-104

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