|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Turbomeca_Arriel_1_E
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
up to 1,000 ° C
|
|
gptkbp:certification
|
EASA certified
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:controls
|
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
modular
|
|
gptkbp:diameter
|
400 mm
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
Brayton cycle
twin-spool
|
|
gptkbp:engine_type
|
three
two
free turbine
|
|
gptkbp:first_flight
|
gptkb:1980
|
|
gptkbp:fuel_capacity
|
200 l/h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
gptkb:full_authority_digital_engine_control_(FADEC)
annular combustion chamber
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Arriel 1 M
|
|
gptkbp:launched
|
starter-generator
|
|
gptkbp:length
|
1,200 mm
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Safran_Helicopter_Engines
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notable_users
|
gptkb:helicopter
|
|
gptkbp:power_output
|
1,000 hp
|
|
gptkbp:propulsion
|
1,000 shp
0.15 kg/hp
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
20,000 ft
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
Eurocopter A S350
|
|
gptkbp:weight
|
150 kg
|