Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
helicopters
|
| gptkbp:category |
aircraft engines
turboshaft engines |
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:developedBy |
gptkb:Turbomeca
|
| gptkbp:firstFlight |
1947
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Artouste engine
|
| gptkbp:introduced |
1947
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:notableFor |
first turboshaft engine to power a production helicopter
|
| gptkbp:powerOutput |
up to 858 shp
|
| gptkbp:status |
retired
|
| gptkbp:type |
single-shaft turboshaft
|
| gptkbp:usedInAircraft |
gptkb:Aérospatiale_Alouette_II
gptkb:Aérospatiale_Alouette_III gptkb:HAL_Chetak gptkb:Westland_Scout gptkb:Westland_Wasp gptkb:HAL_Cheetah |
| gptkbp:variant |
Artouste I
Artouste II Artouste III |
| gptkbp:bfsParent |
gptkb:Turbomeca
|
| gptkbp:bfsLayer |
7
|