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Artouste II C1

Artouste II C1 is a turboshaft engine model used in aircraft.

Specifications

Engine Family: turboshaft

Compressor stages: 1

Dry weight: 163 kilogram

Height: 0.68 metre

Length: 1.48 metre

Max. continuous power: 246 kilowatt

Max. takeoff power: 298 kilowatt

Power turbine stages: 2

Width: 0.76 metre

Manufacturer

Safran Helicopter Engines