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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:application
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civil and military helicopters
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|
gptkbp:average_temperature
|
up to 1,000 ° C
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|
gptkbp:certification
|
EASA and FAA certified
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gptkbp:combustor_type
|
annular combustion chamber
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|
gptkbp:compression_ratio
|
16:1
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gptkbp:control_system
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gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
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gptkbp:cooling_system
|
air-cooled
oil-based coolant
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gptkbp:design
|
modular design
up to 20,000 hours
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gptkbp:development
|
developed from Makila 2 A engine
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gptkbp:diameter
|
600 mm
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gptkbp:emissions_standard
|
low
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gptkbp:engine_configuration
|
horizontal configuration
flexible engine mount system
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gptkbp:engine_power
|
optimized for high altitude performance
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gptkbp:engine_type
|
single-spool engine
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gptkbp:exhaust_system
|
axial exhaust
variable area intake
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gptkbp:first_flight
|
gptkb:2005
|
|
gptkbp:fuel_capacity
|
up to 1,500 liters
|
|
gptkbp:fuel_economy
|
high
200 liters/hour
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
dual fuel system
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|
gptkbp:gearbox
|
integrated reduction gearbox
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Makila 1 M engine
|
|
gptkbp:investment
|
up to 30 bar
|
|
gptkbp:is_tested_for
|
extensively tested in various conditions
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|
gptkbp:launch_date
|
less than 30 seconds
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gptkbp:launch_platform
|
starter-generator
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gptkbp:length
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1,200 mm
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|
gptkbp:maintenance
|
1,500 hours
|
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gptkbp:manufacturer
|
gptkb:Safran_Helicopter_Engines
|
|
gptkbp:market_segment
|
commercial aviation
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_range
|
up to 600 nautical miles
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:operational_use
|
search and rescue missions
|
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gptkbp:power_output
|
1,800 shaft horsepower
|
|
gptkbp:propulsion
|
1,800 shp
6 hp/kg
|
|
gptkbp:reliability
|
high
|
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gptkbp:service_ceiling
|
up to 20,000 feet
|
|
gptkbp:turbine_cooling
|
air-cooled turbine blades
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gptkbp:turbine_speed
|
up to 40,000 RPM
|
|
gptkbp:turbine_type
|
ceramic matrix composites
nickel-based superalloy
two-stage gas generator turbine
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|
gptkbp:type
|
turbo-shaft
|
|
gptkbp:used_in
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gptkb:Eurocopter_EC225_Super_Puma
|
|
gptkbp:warranty
|
standard warranty of 5 years
|
|
gptkbp:weight
|
about 300 kg
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gptkbp:bfsParent
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gptkb:Safran_Helicopter_Engines
|
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gptkbp:bfsLayer
|
5
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