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Contents

   



(Top)
 


1 Specifications  





2 See also  





3 References  














Mil V-7






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From Wikipedia, the free encyclopedia
 


V-7
Role Experimental tip-drive helicopter
Manufacturer Mil
First flight 1959
Introduction 1958

The Mil V-7 was an experimental four-seat helicopter with AI-7 ramjets at the tips of the two rotor blades.[1] It had an egg-shaped fuselage, skid undercarriage, and a two-bladed tail rotor on a short tubular tail boom. Four aircraft were built in the late 1950s, but only one is known to have flown, with only the pilot aboard.[2]

Specifications[edit]

Data from The Osprey Encyclopaedia of Russian Aircraft 1875–1995[2]

General characteristics

See also[edit]

References[edit]

  1. ^ Simpson, R.W. (1998). Airlife's helicopters and rotorcraft. Shrewsbury: Airlife. ISBN 978-1853109683.
  • ^ a b Gunston, Bill (1995). The Osprey Encyclopaedia of Russian Aircraft 1875–1995. London: Osprey. p. 235. ISBN 1-85532-405-9.

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Mil_V-7&oldid=1208971160"

    Categories: 
    1950s Soviet experimental aircraft
    Abandoned military aircraft projects of the Soviet Union
    Mil aircraft
    1950s Soviet helicopters
    Tipjet-powered helicopters
    Ramjet-powered aircraft
    Aircraft first flown in 1959
    Hidden categories: 
    Articles with short description
    Short description matches Wikidata
    Aircraft specs templates hiding performance section
    Commons category link is on Wikidata
     



    This page was last edited on 19 February 2024, at 18:39 (UTC).

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