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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:application
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gptkb:civil_aviation
gptkb:military_aircraft
|
|
gptkbp:average_temperature
|
up to 1,000 ° C
|
|
gptkbp:certification
|
EASA certified
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gptkbp:compressor_type
|
axial compressor
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gptkbp:configuration
|
free turbine
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gptkbp:control_system
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gptkb:FADEC
|
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gptkbp:cooling_system
|
gptkb:oil
air-cooled
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gptkbp:design_feature
|
modular design
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|
gptkbp:diameter
|
600 mm
|
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gptkbp:emissions_standard
|
ICAO Chapter 4
|
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gptkbp:first_flight
|
gptkb:1980
|
|
gptkbp:fuel_economy
|
200 kg/h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
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gptkbp:gearbox
|
reduction gearbox
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gptkbp:history
|
developed in the 1970s
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca Makila
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gptkbp:launch_platform
|
electrical starter
|
|
gptkbp:length
|
1,200 mm
|
|
gptkbp:maintenance
|
3,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Safran_Helicopter_Engines
|
|
gptkbp:market_segment
|
helicopter engines
|
|
gptkbp:notable_users
|
gptkb:British_Army
gptkb:French_Army
gptkb:Royal_Canadian_Air_Force
gptkb:Australian_Army
gptkb:Brazilian_Air_Force
|
|
gptkbp:power_output
|
1,500 shp
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
15,000 feet
|
|
gptkbp:turbine_type
|
single-stage turbine
|
|
gptkbp:type
|
turbo-shaft
|
|
gptkbp:used_in
|
gptkb:Eurocopter_EC225_Super_Puma
gptkb:Eurocopter_AS332_Super_Puma
|
|
gptkbp:variant
|
gptkb:Makila_1_A
gptkb:Makila_2_A1
gptkb:Makila_2_B
gptkb:Makila_2_B1
Makila 2 A
|
|
gptkbp:weight
|
about 300 kg
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_Turbomeca_Adour
|
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gptkbp:bfsLayer
|
6
|