HTS900-2-1D is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Output shaft RPM: 6317
Compressor stages: 2
Control system: FADEC
Dry weight: 153 kilogram
Gas generator stages: 1
Max. continuous power: 564 kilowatt
Max. continuous torque: 85.28 decanewton-metre
Max. takeoff power: 611 kilowatt
Max. takeoff torque: 92.47 decanewton-metre
Max. transient overtorque: 103.04 decanewton-metre
Ng RPM: 47870
Power turbine stages: 1
