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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
civil helicopters
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gptkbp:average_temperature
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up to 1,000 ° C
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gptkbp:certification
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EASA certified
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gptkbp:compression_ratio
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16:1
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gptkbp:controls
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gptkb:football_match
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
digital control system
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gptkbp:cooling_system
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air-cooled
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gptkbp:date
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1970s
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gptkbp:design
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5,000 hours
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gptkbp:diameter
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600 mm
400 mm
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gptkbp:drivetrain
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reduction gearbox
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gptkbp:elevation
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up to 20,000 ft
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gptkbp:emissions_standard
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single exhaust
ICAO Chapter 4
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gptkbp:engine
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twin-spool
free turbine
flexible mount
hot start
cool down procedure
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gptkbp:engine_type
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2
nickel-based superalloy
Makila 1 A1, Makila 2 A2
multi-spool engine
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gptkbp:first_flight
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gptkb:1980
gptkb:1990
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gptkbp:fuel_capacity
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high
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 2 A1
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gptkbp:is_tested_for
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ground testing
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gptkbp:launched
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starter-generator
electrical starter
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gptkbp:length
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1,200 mm
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gptkbp:maintenance
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1,500 hours
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gptkbp:manufacturer
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gptkb:Turbomeca
gptkb:Safran_Helicopter_Engines
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gptkbp:noise_level
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85 d B
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gptkbp:notable_users
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gptkb:military_officer
gptkb:Australian_Army
gptkb:Brazilian_Air_Force
gptkb:Canadian_Forces
gptkb:military_base
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gptkbp:operational_range
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1,000 km
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gptkbp:power_output
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1,800 shp
1,500 k W
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gptkbp:propulsion
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10:1
9:1
1,800 shp
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gptkbp:service_ceiling
|
15,000 ft
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gptkbp:type
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gptkb:engine
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gptkbp:used_in
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Eurocopter E C725 Caracal
Eurocopter A S332 Super Puma
Eurocopter E C225 Super Puma
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gptkbp:weight
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150 kg
200 kg
250 kg
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gptkbp:bfsParent
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gptkb:Turbomeca_Makila_1_A1
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gptkbp:bfsLayer
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6
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