Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb: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
|
| 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:SA_315B_Lama
gptkb:Cheetah_helicopter gptkb:Chetak_helicopter gptkb:IAR_316 gptkb:IAR_316B |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Artouste IIIB
|