Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:diameter |
0.53 m
|
| gptkbp:firstFlight |
1957
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turboméca Artouste IIIB
|
| gptkbp:introduced |
1957
|
| gptkbp:length |
1.36 m
|
| gptkbp:manufacturer |
Turboméca
|
| gptkbp:powerOutput |
~420 shp
|
| gptkbp:successor |
Turboméca Astazou
|
| gptkbp:type |
single-shaft turboshaft
|
| gptkbp:usedInAircraft |
gptkb:Aérospatiale_Alouette_II
gptkb:Aérospatiale_Alouette_III gptkb:HAL_Chetak gptkb:HAL_Cheetah |
| gptkbp:weight |
170 kg
|
| gptkbp:bfsParent |
gptkb:Alouette_III
gptkb:Sud_Aviation_SA_316B_Alouette_III gptkb:Aérospatiale_Alouette_III gptkb:Aérospatiale_SA_316_Alouette_III |
| gptkbp:bfsLayer |
6
|