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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Arriel_2_B
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:controls
|
gptkb:football_match
digital control system
|
|
gptkbp:cooling_system
|
gptkb:engine
air-cooled
|
|
gptkbp:design
|
5000 hours
|
|
gptkbp:diameter
|
0.5 m
|
|
gptkbp:emissions_standard
|
EPA Tier 4
low noise exhaust
|
|
gptkbp:engine
|
gptkb:Arriel_2
42000
650 shp
twin-spool
flexible mount
0.3 m³
|
|
gptkbp:engine_type
|
gptkb:engine
turboshaft
turbo-shaft
nickel alloy
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_capacity
|
0.5 m
1.2 m
150 kg
0.6 m
0.5 kg/k W·h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
annular combustor
dual fuel system
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Arriel 1
|
|
gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:length
|
1.2 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Bell_Helicopter
|
|
gptkbp:market_segment
|
helicopter engines
|
|
gptkbp:max_speed
|
42000
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_range
|
1000 km
|
|
gptkbp:power_output
|
650 shp
|
|
gptkbp:propulsion
|
4.3:1
3.25 k W/kg
|
|
gptkbp:service_ceiling
|
6000 m
|
|
gptkbp:setting
|
free turbine
|
|
gptkbp:torque
|
700 Nm
|
|
gptkbp:type
|
gptkb:engine
electric starter
|
|
gptkbp:used_in
|
gptkb:Bell_429
gptkb:Bell_407
|
|
gptkbp:weight
|
150 kg
200 kg
|