gptkbp:instanceOf
|
turbojet engine
|
gptkbp:aircraft
|
gptkb:Aérospatiale_SA_341_Gazelle
gptkb:Aérospatiale_SA_315_Lama
Aérospatiale_SA_330_Puma
Sud_Aviation_SE_3130_Alouette_II
Sud_Aviation_SE_3160_Alouette_III
|
gptkbp:application
|
helicopter propulsion
|
gptkbp:climate
|
up to 800 °C
|
gptkbp:controls
|
mechanical
|
gptkbp:coolingSystem
|
air-cooled
|
gptkbp:design_feature
|
simple and robust
|
gptkbp:diameter
|
0.3 m
|
gptkbp:drivetrain
|
reduction gearbox
|
gptkbp:emissionsStandard
|
low
|
gptkbp:engineType
|
axial
single-stage
|
gptkbp:firstFlight
|
1950s
|
gptkbp:fuel_capacity
|
0.5 kg/s
|
gptkbp:fuelType
|
annular
spark plug
kerosene
|
gptkbp:historical_significance
|
first French turbojet engine for helicopters
|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca Artouste
|
gptkbp:influenced
|
Whittle_engine_design
|
gptkbp:introduced
|
1950
|
gptkbp:is_used_in
|
gptkb:Aérospatiale_Alouette_III
gptkb:Aérospatiale_Alouette_II
|
gptkbp:launchSite
|
electric starter
|
gptkbp:legacy
|
foundation_for_future_Turbomeca_engines
|
gptkbp:length
|
1.2 m
|
gptkbp:maintenance
|
500 hours
|
gptkbp:manufacturer
|
gptkb:Turbomeca
|
gptkbp:market_segment
|
light helicopters
|
gptkbp:noise_level
|
moderate
|
gptkbp:notable_feature
|
Artouste II
Artouste III
|
gptkbp:operational_status
|
military and civilian
|
gptkbp:origin
|
gptkb:France
|
gptkbp:produces
|
over 1000 units
|
gptkbp:productionYears
|
1940s to 1950s
|
gptkbp:propulsion
|
500 lbf
4.2_lbf/hp
|
gptkbp:reliability
|
high
|
gptkbp:status
|
retired from production
|
gptkbp:successor
|
gptkb:Turbomeca_Astazou
|
gptkbp:type
|
turbojet
|
gptkbp:weight
|
120 kg
|