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Contents

   



(Top)
 


1 See also  





2 References  





3 External links  














Kamov V-100






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From Wikipedia, the free encyclopedia
 


V-100
Role twin-rotor combat helicopter
National origin Russia
Manufacturer Kamov
Status Cancelled design study

The V-100 was a projected side-by-side twin-rotor compound helicopter combat aircraft from Kamov. It had a pusher propeller located behind the rear tailplane, rotors mounted on the tips of its wings and two turbines mounted above the central fuselage, to have the aircraft exceed a projected speed of 400 km/h.[1][2] Integral gun armament was planned to consist of two mobile AO-9 single barrel derivatives of the GSh-23 (one on each side) or a single fixed AO-10 (early version of the GSh-30-1). Other weapons would have included the Kh-25 missile and other stores on two high capacity fuselages and a total of six underwing hardpoints with a combined warload of up to 3000 kg. This project was abandoned and only one model of the aircraft exists.

See also

[edit]

Related development

Aircraft of comparable role, configuration, and era

References

[edit]
  1. ^ V-100, Global Security, accessed 11.03/2021
  • ^ Kamov N.I., accessed 11.03.2021
  • [edit]
    Retrieved from "https://en.wikipedia.org/w/index.php?title=Kamov_V-100&oldid=1228683950"

    Categories: 
    1980s Soviet attack aircraft
    Kamov aircraft
    1980s Soviet helicopters
    Abandoned military aircraft projects of the Soviet Union
    Compound helicopters
    Transverse rotor helicopters
    Hidden categories: 
    Articles with short description
    Short description matches Wikidata
     



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