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Contents

   



(Top)
 


1 Design and development  





2 See also  





3 References  





4 External links  














Yakovlev Yak-45






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From Wikipedia, the free encyclopedia
 


Yak-45
Role Fighter
National origin Soviet Union
Manufacturer Yakovlev
Status Project only
Number built 0

Yakovlev Yak-45 was the designation for a series of design studies in 1973-1974 for a single-seat fighter. It lost to the Mikoyan MiG-29.[1]

Design and development[edit]

In the early 1970s the Soviet VVS expressed a desire to replace the MiG-21 with a more modern twin-engine fighter with greater air-superiority capabilities. Yakovlev's entry was a series of designs submitted under the designation Yak-45.[1]

The Yak-45 would have been powered by two Favorski Type 69 non-vectoring turbofan engines with afterburners. Derived from the R-28, they were rated at 8,000 kg (17,635 lb) thrust each. The engines would have been positioned ahead of a large delta wing, with an additional large canard foreplane, giving the aircraft an appearance similar to the Saab Viggen.[1]

The design was rejected in favor of the MiG-29.[1]

In 1978-1979 Yakovlev attempted to restart development of the Yak-45 by designing a V/STOL version with two vectoring-thrust nozzles and two RD-38 jets. This aircraft was not developed because the problem of roll associated with the loss of one engine during VTOL operation was never solved.[1]

See also[edit]

References[edit]

  1. ^ a b c d e Gunston, 1997

External links[edit]


Retrieved from "https://en.wikipedia.org/w/index.php?title=Yakovlev_Yak-45&oldid=1079654098"

Categories: 
Abandoned military aircraft projects of the Soviet Union
Canard aircraft
Delta-wing aircraft
Yakovlev aircraft
VTOL aircraft
Aircraft with auxiliary jet engines
Hidden categories: 
Articles needing additional references from March 2011
All articles needing additional references
Articles with short description
Short description matches Wikidata
 



This page was last edited on 27 March 2022, at 23:12 (UTC).

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