Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
helicopter propulsion
|
| gptkbp:compressor_type |
axial
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:country_of_origin |
gptkb:France
|
| gptkbp:diameter |
0.3 m
|
| gptkbp:engine_configuration |
turbojet
|
| gptkbp:first_flight |
1950
|
| gptkbp:fuel_type |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Artouste
|
| gptkbp:introduced |
1950s
|
| gptkbp:length |
1.2 m
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:number_of_engines |
gptkb:1
|
| gptkbp:propulsion |
500 lbf
|
| gptkbp:successor |
gptkb:Turbomeca_Astazou
|
| gptkbp:turbine_type |
single-stage
|
| gptkbp:type |
turbojet
|
| gptkbp:used_in |
gptkb:Aérospatiale_Alouette_III
gptkb:Aérospatiale_Alouette_II |
| gptkbp:weight |
120 kg
|
| gptkbp:bfsParent |
gptkb:Turbomeca_Turmo
gptkb:Turbomeca_Astazou |
| gptkbp:bfsLayer |
7
|