Makila 1A1

Engine model
Manufacturer Safran Helicopter Engines
Engine type Turboshaft

Technical specifications

Design
Compressor stages
4
Control system Hybrid hydromechanical + analogue electronic
Gas generator stages
2
Power turbine stages
2
Dimensions
Height
0.67 m
2.2 ft
Length
2.12 m
6.96 ft
Width
0.5 m
1.64 ft
Power limits
Max. continuous power
1,185 kW
1,589 hp
Max. takeoff power
1,357 kW
1,820 hp
Rotation speeds
N1 RPM
33,200
N2 RPM
22,850
Weights
Dry weight
241 kg
531 lb