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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:helicopter
helicopters
civil helicopters
helicopter propulsion
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|
gptkbp:armament
|
2
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
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gptkb:FADEC
digital electronic control
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|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
600 mm
400 mm
|
|
gptkbp:elevation
|
6,000 m
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:Turbomeca
2
helicopters
electric starter
starter-generator
helicopter propulsion
|
|
gptkbp:engine_configuration
|
gptkb:1
free turbine
single-shaft
|
|
gptkbp:engine_cooling_type
|
air-cooled
|
|
gptkbp:engine_max_rpm
|
42,000 rpm
|
|
gptkbp:engine_max_torque
|
1,200 Nm
|
|
gptkbp:engine_maximum_rpm
|
42,000 rpm
|
|
gptkbp:engine_number_of_blades
|
2
|
|
gptkbp:engine_power
|
1,800 shp
1,500 shp
10 shp/kg
|
|
gptkbp:engine_thrust_to_weight_ratio
|
10:1
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
turbo-shaft
|
|
gptkbp:first_flight
|
gptkb:1980
|
|
gptkbp:fuel_capacity
|
150 kg
250 kg
1,200 mm
600 mm
400 mm
|
|
gptkbp:fuel_economy
|
200 kg/h
0.5 kg/s
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca Makila 1 A
|
|
gptkbp:launch_window
|
electric starter
starter-generator
|
|
gptkbp:length
|
1,200 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Turbomeca
|
|
gptkbp:maximum_rpm
|
42,000 rpm
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:power_output
|
1,500 shp
1,500 k W
|
|
gptkbp:powers
|
10 shp/kg
|
|
gptkbp:propulsion
|
10:1
1,800 shp
6.0 k W/kg
|
|
gptkbp:service_ceiling
|
6,000 m
|
|
gptkbp:service_entry
|
gptkb:1980
|
|
gptkbp:turbine_type
|
single-stage turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Eurocopter_EC225_Super_Puma
gptkb:Eurocopter_AS332_Super_Puma
|
|
gptkbp:weight
|
150 kg
250 kg
300 kg
|
|
gptkbp:bfsParent
|
gptkb:Eurocopter_Tiger
|
|
gptkbp:bfsLayer
|
5
|