Astazou XII H1 is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 3
Dry weight: 158 kilogram
Length: 1.47 metre
Max. continuous power: 470 kilowatt
Max. takeoff power: 470 kilowatt
Output shaft RPM: 2066
Power turbine stages: 3
ICAO: SC7
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