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By
Wikipedia,
the free encyclopedia,
http://en.wikipedia.org/wiki/Tupolev_Tu-124
The Tupolev Tu-124 (NATO codename: Cookpot) was a Soviet short range twinjet airliner capable of carrying 56 passengers.
Design and development
Developed from the medium-range Tupolev Tu-104, the Tu-124 was meant to meet Aeroflot's requirement for a regional airliner to supersede the Ilyushin Il-14. It was very similar to the Tu-104 (merely a scaled-down version). The two were hard to tell apart when seen at a distance. It was not a complete copy of the Tu-104, however. The Tu-124 included a number of refinements, including double-slotted flaps, a large centre-section airbrake, automatic spoilers, and the extension of the wings' trailing edge roots. It also included a drogue parachute to be used in the event of an emergency landing or landing on a slippery surface and low pressure tires in the event of a rough landing surface. It also boosted fuel efficiency, being the first short-range aircraft fitted with turbofans.
Competition with COMECON
DDR competed within COMECON trading block with a four-engined design called Baade B-152 the design was halted and Interflug bought Tu-134 instead.
Variants
- Tu-124/Tu-124V
- The first production variant. The international demand for it was small, because most foreign airlines were waiting to buy the improved Tupolev Tu-134.
- Tu-124K/Tu-124K2
- These were the VIP configuration. They were operated by the militaries of Iraq and China, and by the Indian Air Force.
- Tu-124Sh-1
- Military version used as navigator trainers.
- Tu-124Sh-2
- Military version used as navigator trainers.
Operators
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Tu-124 operators (countries with only military operators in dark red) |
Civil operators
Czechoslovakia
East Germany
- Interflug (operated in Interflug colours, but owned by East German Airforce)
Iraq
Soviet Union
Military operators
People's Republic of China
Czechoslovakia
East Germany
India
Iraq
Soviet Union
Specifications (Tu-124V)General characteristics
- Crew: three
- Capacity: 56 passengers
- Length: 30.58 m (100 ft 4 in)
- Wingspan: 25.55 m (83 ft 10 in)
- Height: 8.08 m (26 ft 6 in)
- Wing area: 119 m² (1,280 ft²)
- Empty weight: 22,500 kg (49,500 lb)
- Useful load: 30,000 kg (67,000 lb)
- Max takeoff weight: 38,000 kg (84,000 lb)
- Powerplant: 2× Soloviev D-20P turbofans, 52.9 kN (11,900 lbf) each
Performance
See also
Related development Tu-16 - Tu-104 - Tu-107 - Tu-110
Comparable aircraft
Related lists List of airliners
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Published in July 2009.
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