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Tupolev Tu-80

Military Aircraft

The Tupolev Tu-80 was a Soviet prototype for a longer-ranged version of the Tu-4 bomber, itself an unlicensed, reverse-engineered copy of the Boeing B-29 Superfortress. Work began in February 1948 on a modernised and enlarged Tu-4 with more fuel-efficient engines, better aerodynamics and extra fuel tanks, aimed at a range of 7,000 to 8,000 km and a bomb load of up to 12,000 kg. The fuselage was lengthened by almost 4 m, the nose was redesigned with an airliner-style stepped windscreen and the wings were enlarged to 173 square metres, with four Shvetsov ASh-73TKFN radial engines. The programme was cancelled in September 1949 in favour of the Tu-85, and the first flight came on 1 December 1949. The sole prototype became a research aircraft testing reversible-pitch propellers and structural deformation in heavy aircraft, and ended its life as a target.

Facts
Year
1949 1
Engine Class
Piston 1
Status
Cancelled 1
Units Built
1 1
Top Speed (km/h)
545 1
Mass (kg)
37,850 1
Maximum Mass (kg)
60,600 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Tupolev Tu-80 (Wikipedia)

Of Make

Source Tupolev Tu-80 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Tupolev Tu-80 (Wikipedia)Lead
Quote, Lead
a longer-ranged version of the Tupolev Tu-4 bomber

Originated In

Also in Geography Atlas: where this subject originated.

Source Tupolev Tu-80 (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
was a Soviet prototype for a longer-ranged version
Sources
1. Tupolev Tu-80 (Wikipedia)
  • Development
    the first flight was not until 1 December 1949
  • Lead
    a longer-ranged version of the Tupolev Tu-4 bomber
  • Lead, status
    It was cancelled in 1949 in favor of the Tupolev Tu-85 program
  • Specifications
    18-cylinder air-cooled radial piston engines, 1,980 kW (2,650 hp)
  • Lead, units built
    The sole prototype
  • Specifications, mass
    Empty weight: 37,850 kg (83,445 lb)
  • Specifications, maximum mass
    Max takeoff weight: 60,600 kg (133,600 lb)
  • Specifications, top speed
    Maximum speed: 545 km/h (339 mph, 294 kn)
  • Lead, country of origin
    was a Soviet prototype for a longer-ranged version
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