Turbomeca Artouste

GPTKB entity

Properties (47)
Predicate Object
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