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Tupolev ANT-25

Supersonic and Experimental Aircraft

The Tupolev ANT-25 was a Soviet long-range experimental aircraft, first constructed in 1933 and used for a series of record-breaking flights. Kliment Voroshilov recommended building an aircraft for long-range flights in December 1931, and a brigade of the TsAGI experimental design department led by Pavel Sukhoi designed it under the overall supervision of Andrei Tupolev. The first prototype made its maiden flight on 22 June 1933 with Mikhail Gromov at the controls, powered by a single Mikulin M-34 engine. Very long, narrow wings gave it exceptional range and held fuel equal to more than half its takeoff weight. In July 1936 Valery Chkalov, Georgy Baydukov and Alexander Belyakov flew one from Moscow to the Far East in 56 hours 20 minutes, and in June 1937 the same crew flew non-stop from Moscow over the North Pole to the United States in 63 hours 25 minutes. Three weeks later Gromov's crew flew a second aircraft to San Jacinto, California. Only two were built, and the military development, the DB-1, was an unsuccessful bomber.

Facts
Year
1933 1
Engine Class
Piston 1
Power (kW)
560 1
Units Built
2 1
Top Speed (km/h)
246 1
Mass (kg)
3700 1
Engine
Mikulin M-34 V-12 liquid-cooled piston engine 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Tupolev ANT-25 (Wikipedia)

Of Make

Source Tupolev ANT-25 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Tupolev ANT-25 (Wikipedia)Development, supervision
Quote, Development, supervision
under the overall supervision of Andrei Tupolev

Originated In

Also in Geography Atlas: where this subject originated.

Source Tupolev ANT-25 (Wikipedia)Lead, origin
Quote, Lead, origin
was a Soviet long-range experimental aircraft
Sources
1. Tupolev ANT-25 (Wikipedia)
  • Development, maiden flight
    made its maiden flight on 22 June 1933
  • Lead, aircraft type
    was a Soviet long-range experimental aircraft
  • Specifications, powerplant
    1 × Mikulin M-34 V-12 liquid-cooled piston engine, 560 kW (750 hp)
  • Specifications, power
    1 × Mikulin M-34 V-12 liquid-cooled piston engine, 560 kW (750 hp)
  • Specifications, empty weight
    Empty weight: 3,700 kg (8,157 lb)
  • Specifications, maximum speed
    Maximum speed: 246 km/h (153 mph, 133 kn)
  • Design, number built
    Only two aircraft were manufactured
  • Development, supervision
    under the overall supervision of Andrei Tupolev
  • Lead, origin
    was a Soviet long-range experimental aircraft
  • Exemplifies: Aviation, Lead, aircraft
    was a Soviet long-range experimental aircraft
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