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gptkbp:instance_of
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gptkb:engine
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gptkbp:bfsLayer
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4
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gptkbp:bfsParent
|
gptkb:Airbus_H130
|
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gptkbp:application
|
civil and military aviation
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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
|
approximately 0.5 m
|
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gptkbp:emissions_standard
|
meets ICAO standards
free power turbine
|
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gptkbp:engine_type
|
axial compressor
single-stage gas generator
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gptkbp:first_introduced
|
gptkb:1980s
|
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gptkbp:fuel_capacity
|
approximately 200 kg/h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
annular combustor
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca Arriel 2 D
|
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gptkbp:launch_site
|
starter-generator
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gptkbp:length
|
approximately 1.2 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Safran_Helicopter_Engines
|
|
gptkbp:max_speed
|
up to 300 knots
|
|
gptkbp:power_output
|
around 500 shp
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
up to 20,000 feet
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
helicopters
|
|
gptkbp:variant
|
gptkb:Arriel_2_B
gptkb:Arriel_2_M
gptkb:Arriel_2_S
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gptkbp:weight
|
approximately 150 kg
|