Makila 1A2 Turbine

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Family
Makila
Aircraft Engine Manufacturer
Safran Helicopter Engines
Aircraft Engine Type
Turboshaft
Comment
AS332L2/AS532
Dry Weight (kg)
247
Length (mm)
2117
Height (mm)
673
Width (mm)
498
Control System
Hybrid hydromechanical / digital electronic (DECU)
Certification
1991-06-06
Modules
4
Fuel
Jet-A1
LP Compressor Stages
0
IP Compressor Stages
0
HP Compressor Stages
4
HP Compressor Technology
3 axial, 1 centrifugal
Combustion Chamber
Annular reverse flow
HP Turbine Stages
2
HP Turbine Technology
axial
IP Turbine Stages
0
LP Turbine Stages
2
LP Turbine Technology
axial
T45 Start (°C)
750
T45 Take Off (°C)
825
T45 Max Continuous (°C)
770
T45OEI Contiuous (°C)
840
Maximum Takeoff Power (kW)
1376
Maximum Continuous Power (kW)
1236
OEI30sec Power (kW)
1573
OEI2min Power (kW)
1467
OEI Continuous Power (kW)
1420
BP Take Off Rotation Speed (rpm)
22962
HP Take Off Rotation Speed (rpm)
33200
Output Clockwise Rotation
No

Related

153 empty fields

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