Walter M601 turboprop aircraft engine

Details: Category: Aero - engines

Walter M601 turboprop aircraft engine © Konstantinos Panitsidis

Photo from the personal collection of Konstantinos Panitsidis

Technical specifications Photos Video Video

TECHNICAL SPECIFICATIONS

Fuel	Kerosene
Oil	-
Propeller shaft power, take-off power rating	750 h.p.
Specific fuel consumption, take-off power rating	0,200 kg/e.h.p.*h
Propeller shaft power, cruise power	-
Specific fuel consumption, cruise power	-
Pressure ratio, take-take-off power rating	-
Temperature of the gas at the turbine intake, take-off power rating	690 ^oC
Air flow rate, take-off power rating	-
Compressor rotation frequency low-pressure, take-off power rating	-
Diameter	590 mm
Height	-
Width	590 mm
Lenght	1675 mm
Weight	197 kg
Specified service life	-

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