Group Information
Last Activity: | 4 Days Ago |
Group Leader: | CollieSmile |
Moderators: |
betseybutler |
Submissions: | Open |
Group Visitors: | 871,597 |
Founded: | May 18th, 2013 |
Top Contributors
Recently Active Members
Recently Joined Members
Tupolev Tu-144
Wallpaper Description:
The Tupolev Tu-144 was the first commercial supersonic transport aircraft (SST).It was one of only two SSTs to enter commercial service, the other being the Anglo-French Concorde.
The design, publicly unveiled in January 1962, was constructed in the Soviet Union under the direction of the Tupolev design bureau, headed by Alexei Tupolev.
The prototype first flew on 31 December 1968 near Moscow, two months before the first flight of Concorde.
The Tu-144 first went supersonic on 5 June 1969, and on 26 May 1970 became the first commercial transport to exceed Mach 2.
The frequent comparisons to Concorde led to the Tu-144 being known as "Concordski" in the West.
A Tu-144 crashed in 1973 at the Paris Air Show, delaying its further development.
The aircraft was introduced into passenger service on 1 November 1977, almost two years after Concorde.
In May 1978, another Tu-144 (an improved version, named Tu-144D) crashed in a test flight while being delivered, and the passenger fleet was permanently grounded after only 55 scheduled flights.
The aircraft remained in use as a cargo plane until 1983, by which point a total of 102 commercial flights had been completed.
The Tu-144 was later used by the Soviet space programme to train pilots of the Buran spacecraft, and by NASA for supersonic research.
General characteristics
• Crew: 3
• Capacity: 140 passengers (11 1-st class & 129 tourist class)
• Length: 65.50 m (215.54 ft)
• Wingspan: 28.80 m (94.48 ft)
• Height: 12.50 m (41.00 ft)
• Wing area: 506.35 m² (5,450 ft²)
• Empty weight: 99,200 kg (218,500 lb)
• Loaded weight: 125,000 kg (275,330 lb)
• Max. takeoff weight: 207,000 kg (455,950 lb)
• Powerplant: 4 × Kolesov RD-36-51 turbojet, 200 kN (44,122 lbf)[N 6] each
Performance
• Cruise speed: Mach 2.15 (2,120 km/h (1,320 mph))
• Service ceiling: 20,000 m (65,600 ft)
• Rate of climb: 3,000 m/min (9,840 ft/min)
• Wing loading: 410.96 kg/m² (84.20 lb/ft²)
• Thrust/weight: 0.44