Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:diameter |
0.53 m
|
| gptkbp:firstFlight |
1951
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Artouste II
|
| gptkbp:length |
1.36 m
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:notableFor |
first turboshaft engine to power a production helicopter
|
| gptkbp:powerOutput |
~400 shp
|
| gptkbp:successor |
Turbomeca Artouste III
|
| gptkbp:type |
single-shaft turboshaft
|
| gptkbp:usedInAircraft |
gptkb:Aérospatiale_Alouette_II
gptkb:Sud-Ouest_Djinn gptkb:Aérospatiale_Lama |
| gptkbp:weight |
150 kg
|
| gptkbp:bfsParent |
gptkb:Sud_Aviation_Alouette_II
gptkb:Sud_Aviation_SE_3130_Alouette_II gptkb:Aérospatiale_SA_318_Alouette_II |
| gptkbp:bfsLayer |
6
|