Mil Mi-1

General Data
First Flown:	1948	Length:	39 ft 4.5 in
Lift Capability:		Height:
Range:		Rotor Span:	47 ft 1 in
Top Speed:	125 mph	Empty Weight:	3,900 lb
Service Ceiling:		Max Gross Weight:	5,300 lb
Engines:	575 PS Ivchenko AI-26V Radial Piston Engine
Armament:	n/a
Accommodations:	3	Cargo:
Operators:	Albania, Bulgaria, China, Cuba, Czechoslovakia, East Germany, Finland, Iraq, Romania and Syria

Similar Aircraft:
Other Features:	NATO reporting name is Hare


Notes
The first prototype flew in 1948 and was the first Russian helicopter to use the classic single rotor layout. Production ended in 1958.

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