TM 333 2M2

Engine model
Manufacturer Safran Helicopter Engines
Engine type Turboshaft

Technical specifications

Design
Compressor stages
3
Control system Single channel EECU
Gas generator stages
1
Power turbine stages
1
Dimensions
Height
0.75 m
2.46 ft
Length
1.05 m
3.44 ft
Width
0.45 m
1.48 ft
Power limits
Max. continuous power
736 kW
987 hp
Max. takeoff power
807 kW
1,082 hp
Rotation speeds
N1 RPM
45,000
N2 RPM
37,562
Output shaft RPM
6,000
Torque limits
Max. continuous torque
108.8 daN/m
802.5 lbf⋅ft
Max. takeoff torque
123 daN/m
907.2 lbf⋅ft
Max. transient overtorque
136 daN/m
1,003.1 lbf⋅ft
Weights
Dry weight
163 kg
359 lb