Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:certification |
gptkb:EASA
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:diameter |
0.39 m
|
| gptkbp:family |
gptkb:Turbomeca_Arrius
|
| gptkbp:firstFlight |
1994
|
| gptkbp:fuelType |
gptkb:Jet-A1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Arrius 2B2
|
| gptkbp:length |
1.1 m
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:marketedAs |
gptkb:Safran_Helicopter_Engines
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:numberOfStages |
2
|
| gptkbp:powerOutput |
633 shp
|
| gptkbp:usedIn |
gptkb:Eurocopter_EC135
|
| gptkbp:weight |
154 kg
|
| gptkbp:bfsParent |
gptkb:Eurocopter_EC135
|
| gptkbp:bfsLayer |
6
|