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TM 333 2M2

TM 333 2M2 is a turboshaft engine model used in aircraft.

Specifications

Engine Family: turboshaft

Compressor stages: 3

Control system: Single channel EECU

Dry weight: 163 kilogram

Gas generator stages: 1

Height: 0.75 metre

Length: 1.05 metre

Max. continuous power: 736 kilowatt

Max. continuous torque: 108.8 decanewton-metre

Max. takeoff power: 807 kilowatt

Max. takeoff torque: 123 decanewton-metre

Max. transient overtorque: 136 decanewton-metre

Ng RPM: 45000

Np RPM: 37562

Output shaft RPM: 6000

Power turbine stages: 1

Width: 0.45 metre

Manufacturer

Safran Helicopter Engines