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gptkbp:instanceOf
|
turbojet engine
|
|
gptkbp:application
|
gptkb:Aérospatiale_SA_319B
gptkb:Aérospatiale_SA_316B
gptkb:Aérospatiale_SA_315B
gptkb:SA_330_Puma
gptkb:SA_341_Gazelle
helicopters
|
|
gptkbp:certifications
|
gptkb:EASA
gptkb:FAA
|
|
gptkbp:climate
|
-40 to 50 °C
|
|
gptkbp:controls
|
hydromechanical
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
Axial-flow
|
|
gptkbp:developer
|
1950s
|
|
gptkbp:diameter
|
0.4 m
|
|
gptkbp:engine
|
low
horizontal
|
|
gptkbp:engineConfiguration
|
single-shaft
|
|
gptkbp:engineType
|
2
1
|
|
gptkbp:firstFlight
|
1956
|
|
gptkbp:fuel_capacity
|
0.5 kg/kW·h
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca Astazou
|
|
gptkbp:is_used_in
|
gptkb:Aérospatiale_SA_315_Lama
|
|
gptkbp:legacy
|
widely used in military helicopters
widely used in civilian helicopters
|
|
gptkbp:length
|
1.2 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Turbomeca
|
|
gptkbp:noise_level
|
85 dB
|
|
gptkbp:notable_feature
|
Astazou II
Astazou III
|
|
gptkbp:operationalHistory
|
in service since 1956
|
|
gptkbp:powerOutput
|
370 kW
|
|
gptkbp:propulsion
|
500 to 1,000 lbf
|
|
gptkbp:related_engine
|
gptkb:Turbomeca_Arriel
gptkb:Turbomeca_TM_319
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
15,000 ft
|
|
gptkbp:successor
|
gptkb:Turbomeca_Arriel_2
gptkb:Turbomeca_Arriel_1
|
|
gptkbp:type
|
turbo-shaft engine
|
|
gptkbp:weight
|
120 kg
|