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gptkbp:instance_of
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gptkb:engine
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|
gptkbp:aircraft_operated
|
gptkb:helicopter
|
|
gptkbp:application
|
gptkb:aircraft
gptkb:helicopter
|
|
gptkbp:average_temperature
|
up to 1,000 ° C
up to 1,050 ° C
|
|
gptkbp:certification
|
EASA certified
|
|
gptkbp:compression_ratio
|
16:1
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gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
modular design
|
|
gptkbp:developer
|
derived from Arriel 1
|
|
gptkbp:diameter
|
400 mm
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
twin-spool
up to 5,000 hours
|
|
gptkbp:engine_type
|
gptkb:engine
free turbine
|
|
gptkbp:first_flight
|
gptkb:1996
|
|
gptkbp:fuel_capacity
|
high
0.5 kg/s
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
annular combustor
dual fuel system
can-type combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Arriel 2 K
|
|
gptkbp:launch_site
|
starter-generator
|
|
gptkbp:legal_issue
|
gas turbine cycle
|
|
gptkbp:length
|
1,200 mm
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Safran_Helicopter_Engines
|
|
gptkbp:market_segment
|
light helicopters
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_area
|
helicopter operations
|
|
gptkbp:power_output
|
500-650 shp
|
|
gptkbp:propulsion
|
650 shp
4.3 shp/kg
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
20,000 ft
|
|
gptkbp:successor
|
gptkb:Arriel_2_E
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
Eurocopter E C135
|
|
gptkbp:weight
|
150 kg
|
|
gptkbp:weight_class
|
lightweight engine
|
|
gptkbp:bfsParent
|
gptkb:Arriel_engine
|
|
gptkbp:bfsLayer
|
6
|