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Yakovlev Yak-140

Supersonic and Experimental Aircraft

The Yakovlev Yak-140 was a Soviet prototype lightweight supersonic fighter developed in the 1950s around the Mikulin AM-11 turbojet, rated at 40 kN dry and 50 kN with afterburner. A 1953 specification required a speed of 1,650 to 1,750 km/h and a range of 1,800 km, with three 30 mm cannon and the ability to carry rockets and 200 kg of bombs. The fighter had a semi-monocoque fuselage, a nose air intake with a range-only radar, wings swept 55 degrees and tandem landing gear. The prototype was completed in 1954 but was denied authorisation for flight testing, and the programme was cancelled in 1956.

Facts
Engine Class
Jet 1
Status
Cancelled 1
Comparison
Body Style
Aircraft (no road body style) 1
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Exemplifies

Aviation, Modes
Source Yakovlev Yak-140 (Wikipedia)

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Source Yakovlev Yak-140 (Wikipedia)
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Source Yakovlev Yak-140 (Wikipedia)Lead, maker
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was a Soviet prototype lightweight supersonic fighter developed during the 1950s

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was a Soviet prototype lightweight supersonic fighter developed during the 1950s
Sources
1. Yakovlev Yak-140 (Wikipedia)
  • Lead, body style
    was a Soviet prototype lightweight supersonic fighter developed during the 1950s
  • Lead, status
    the program was cancelled in 1956
  • Development, engine
    developed around the Mikulin AM-11 turbojet
  • Lead, maker
    was a Soviet prototype lightweight supersonic fighter developed during the 1950s
  • Lead, country of origin
    was a Soviet prototype lightweight supersonic fighter developed during the 1950s
  • In Group: High-Speed Military Prototypes and Reconnaissance Aircraft, Lead, kind of aircraft
    was a Soviet prototype lightweight supersonic fighter developed during the 1950s
  • Exemplifies: Aviation, Lead, mode
    was a Soviet prototype lightweight supersonic fighter developed during the 1950s
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