Statements (20)
Predicate | Object |
---|---|
gptkbp:instanceOf |
piston engine
|
gptkbp:application |
gptkb:helicopter
|
gptkbp:compressionRatio |
centrifugal compressor
|
gptkbp:countryOfOrigin |
gptkb:France
|
gptkbp:diameter |
0.48 m
|
gptkbp:firstFlight |
1957
|
gptkbp:fuelType |
kerosene
|
https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Artouste IIIB
|
gptkbp:length |
1.36 m
|
gptkbp:manufacturer |
gptkb:Turbomeca
|
gptkbp:powerOutput |
~420 shp
|
gptkbp:status |
out of production
|
gptkbp:successor |
Turbomeca Artouste IIID
|
gptkbp:type |
single-shaft turboshaft
|
gptkbp:usedInAircraft |
gptkb:Aérospatiale_Alouette_II
gptkb:Aérospatiale_Alouette_III gptkb:HAL_Chetak |
gptkbp:weight |
170 kg
|
gptkbp:bfsParent |
gptkb:Chetak_helicopter
|
gptkbp:bfsLayer |
5
|