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Mil V-8

mi_v8


The Mi-8 prototype incorporating an Mi-4 main rotor and transmission and one 2700shp Soloviev AI-24V turbine mounted on top of fuselage. First flown on 24 June 1961 and subsequently fitted with 5-blade rotor and two 1400shp Isotov TV2-117 engines, being the standard for the Mi-8.

V-8
Crew: 3
Passengers: 18
Engine: 1 x AI-24V turboshaft, 1425kW
Main rotor diameter: 21.0m
Max take-off weight: 11200kg
Empty weight: 5726kg
Payload: 1500-2000kg

mi_v8

 

 

 

 


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