Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
single-shaft
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:diameter |
0.39 m
|
| gptkbp:family |
gptkb:Turbomeca_Arriel
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Arriel 1B
|
| gptkbp:length |
1.24 m
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:powerOutput |
641 shp
|
| gptkbp:status |
in service
|
| gptkbp:usedIn |
gptkb:Eurocopter_AS350_B2
|
| gptkbp:weight |
155 kg
|
| gptkbp:bfsParent |
gptkb:Aérospatiale_AS350BA_Écureuil
gptkb:Aérospatiale_AS350B_Écureuil |
| gptkbp:bfsLayer |
6
|