H85-200 is a turboprop engine model used in aircraft.
Engine Family: turboprop
Compressor stages: 3
Control system: Hydromechanical
Dry weight: 202 kilogram
Gas generator stages: 1
Height: 0.65 metre
Length: 1.68 metre
Max. continuous power: 634 kilowatt
Max. takeoff power: 634 kilowatt
Ng RPM: 36660
Np RPM: 30960
Output shaft RPM: 1950
Power turbine stages: 1
Width: 0.59 metre
ICAO: -
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