Jump to content

Kamov V-100

From Alfawiki
Adapted from the English Wikipedia article Kamov V-100, available under CC BY-SA 4.0Updated 29 November 2025
Kamov
IndustryAerospace
Headquarters
Soviet Union
ProductsHelicopters, aircraft

Template:Infobox aircraft

The V-100 represented a conceptual combat compound helicopter designed by Kamov, featuring a side-by-side twin-rotor configuration. It was intended to incorporate rotors positioned at the extremities of its wings, with two turbines installed above the central fuselage. Additionally, a pusher propeller was planned to be mounted aft of the rear tailplane, aiming to enable the aircraft to surpass a forecasted velocity of 400 km/h. The armament design included two maneuverable AO-9 single-barrel guns—derivatives of the Gryazev-Shipunov GSh-23—installed on either side, or alternatively, a single fixed AO-10 (an early variant of the GSh-30-1). The weapons suite was expected to be supplemented by Kh-25 missiles and other ordnance carried on two spacious fuselage stations, along with six underwing hardpoints capable of supporting an aggregate payload of up to 3000 kg. This initiative did not progress beyond the conceptual phase, with only one prototype model constructed.

See also

Template:Aircontent

References

External links

Template:Kamov aircraft