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
Engine Class Top Speed (km/h) Maximum Mass (kg) EngineTumansky R-79V-300 afterburning vectoring-nozzle turbofan 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Yakovlev Yak-141 (Wikipedia)
Of Make
Source Yakovlev Yak-141 (Wikipedia)
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Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Yakovlev Yak-141 (Wikipedia)LeadQuote, 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)LeadQuote, 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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