Makila 2A Turbine

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Family
Makila
Aircraft Engine Manufacturer
Safran Helicopter Engines
Aircraft Engine Type
Turboshaft
Dry Weight (kg)
278.9
Length (mm)
2115
Height (mm)
668
Width (mm)
785
Control System
FADEC Dual Channel
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)
780
T45 Take Off (°C)
796
T45 Max Continuous (°C)
749
T45OEI Contiuous (°C)
799
Maximum Takeoff Power (kW)
1303
Maximum 30min Power (kW)
1303
Maximum Continuous Power (kW)
1303
OEI30sec Power (kW)
1758
OEI2min Power (kW)
1660
OEI Continuous Power (kW)
1573
BP Take Off Rotation Speed (rpm)
22962
HP Take Off Rotation Speed (rpm)
33200
Output Clockwise Rotation
No

Related

154 empty fields

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