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Yakovlev Yak-141

Supersonic and Experimental Aircraft

The Yakovlev Yak-141, also designated Yak-41 and given the NATO reporting name Freestyle, was a Soviet supersonic vertical and short takeoff and landing fighter designed by the Yakovlev bureau to replace the subsonic Yak-38 aboard Soviet aircraft carriers. After studying twin-engine layouts and rejecting them because an engine failure during landing would cause asymmetric thrust, the designers chose a single main engine, a Tumansky R-79V-300 with a vectoring nozzle, backed by two Rybinsk RD-41 lift jets behind the cockpit. Four prototypes were built, two of them used for flight testing. The first flight was made at Zhukovsky on 9 March 1987, and in September 1991 the type made its first landings aboard the carrier Admiral Gorshkov. Funding collapsed after the Soviet Union dissolved and the project was cancelled, although a partnership with Lockheed was announced in 1992 and surviving airframes are displayed in Russian museums.

Facts
Year
1987 1
Engine Class
Jet 1
Status
Cancelled 1
Units Built
4 1
Top Speed (km/h)
1800 1
Mass (kg)
11,650 1
Maximum Mass (kg)
19,500 1
Engine
Tumansky R-79V-300 afterburning vectoring-nozzle turbofan 1
Comparison
Body Style
Aircraft (no road body style) 1
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Aviation, Modes
Source Yakovlev Yak-141 (Wikipedia)

Of Make

Source Yakovlev Yak-141 (Wikipedia)
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Source Yakovlev Yak-141 (Wikipedia)Lead
Quote, Lead
is a Soviet supersonic vertical takeoff/landing (VTOL) fighter aircraft designed by Yakovlev

Originated In

Also in Geography Atlas: where this subject originated.

Source Yakovlev Yak-141 (Wikipedia)Lead
Quote, Lead
is a Soviet supersonic vertical takeoff/landing (VTOL) fighter aircraft designed by Yakovlev
Sources
1. Yakovlev Yak-141 (Wikipedia)
  • Lead
    is a Soviet supersonic vertical takeoff/landing (VTOL) fighter aircraft designed by Yakovlev
  • History, first flight
    The first flight took place on in 9 March 1987 at Zhukovsky
  • Specifications, powerplant
    Powerplant: 1 × Tumansky R-79V-300 afterburning vectoring-nozzle turbofan, 108 kN (24,000 lbf) thrust dry, 152 kN (34,000 lbf) with afterburner
  • Specifications, engine fitted
    Powerplant: 1 × Tumansky R-79V-300 afterburning vectoring-nozzle turbofan, 108 kN (24,000 lbf) thrust dry, 152 kN (34,000 lbf) with afterburner
  • Specifications, empty weight
    Empty weight: 11,650 kg
  • Specifications, maximum weight
    Max takeoff weight: 19,500 kg
  • Specifications, maximum speed
    Maximum speed: 1,800 km/h
  • Status
    Four prototypes were built before the project's cancellation.
  • Production, number built
    Four prototypes were built
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