Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:certification |
gptkb:EASA
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:family |
gptkb:Turbomeca_Arriel
|
| gptkbp:firstFlight |
1997
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Arriel 2B
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:numberOfAxles |
1
|
| gptkbp:powerOutput |
847 shp
|
| gptkbp:status |
in production
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:Eurocopter_AS350_B3
|
| gptkbp:bfsParent |
gptkb:Aérospatiale_AS350B3_Écureuil
gptkb:Aérospatiale_AS550C3_Fennec |
| gptkbp:bfsLayer |
6
|