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gptkbp:instance_of
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gptkb:engine
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gptkbp:application
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gptkb:helicopter
helicopters
civil helicopters
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gptkbp:average_temperature
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-40 to 50 ° C
650 ° C
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gptkbp:compression_ratio
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16:1
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gptkbp:controls
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gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
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gptkbp:cooling_system
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air-cooled
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gptkbp:diameter
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400 mm
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gptkbp:drivetrain
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reduction gearbox
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gptkbp:emissions_standard
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ICAO Chapter 4
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gptkbp:engine
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gptkb:Makila_series
civil and military use
1,500 shp
free turbine
starter-generator
flexible mount
single spool
nickel-based superalloy
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gptkbp:engine_type
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single-spool
free turbine
axial compressor
turbo-shaft
nickel-based superalloy
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gptkbp:first_flight
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gptkb:1980
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gptkbp:fuel_capacity
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150 kg
1,200 mm
400 mm
200 kg/h
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gptkbp:fuel_type
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gptkb:Jet_A-1
annular combustor
annular combustion chamber
dual fuel system
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https://www.w3.org/2000/01/rdf-schema#label
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Turbomeca Makila 1 A1
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gptkbp:ignition_system
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spark ignition
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gptkbp:launch_site
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starter-generator
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gptkbp:length
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1,200 mm
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gptkbp:maintenance
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500 hours
1,500 hours
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gptkbp:manufacturer
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gptkb:Turbomeca
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gptkbp:max_speed
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300 km/h
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gptkbp:noise_level
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85 d B
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gptkbp:number_of_stages
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2
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gptkbp:operational_range
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1,000 km
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gptkbp:origin
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gptkb:Monarch
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gptkbp:power_output
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1,500 shp
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gptkbp:propulsion
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1,500 shp
10 shp/kg
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gptkbp:service_ceiling
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6,000 m
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gptkbp:successor
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gptkb:Turbomeca_Makila_2_A1
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gptkbp:type
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gptkb:engine
electrical starter
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gptkbp:used_in
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Eurocopter A S332 Super Puma
Eurocopter E C225 Super Puma
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gptkbp:weight
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150 kg
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gptkbp:bfsParent
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gptkb:Tigre_ARH
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gptkbp:bfsLayer
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5
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