Mi-8 prototype incorporating Mi-4 main rotor and transmission and one 2700shp Soloviev AI-24V turbine mounted on top of fuselage. First flown on 24 June 1961. Subsequently fitted with 5-blade rotor and two 1400shp Isotov TV2-117 engines.
|Technical data for V-8
engine: 1 x AI-24V turboshaft, rated at 1425kW,
main rotor diameter: 21.0m,
take-off weight: 11200kg,
empty weight: 5726kg,
|flyboard.info, e-mail, 22.08.2011||reply|
ALL ANNOUNCING AVIATION of flyboard.info
|x x, e-mail, 10.12.2013||reply|
obvious front liner air liner no imitations available originals only or?
|Bo3Dyx, e-mail, 10.07.2008||reply|
Лучшия машина в мире!
|zolghadri, e-mail, 25.04.2008||reply|
A great job that aerospace enthusiasts will surely cherish
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