Statements (14)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
helicopter engine
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:firstFlight |
1980s
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:partOfSeries |
gptkb:Turbomeca_Arriel
|
| gptkbp:powerOutput |
~840 shp
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedInAircraft |
gptkb:Eurocopter_AS365_Dauphin
gptkb:Harbin_Z-9 |
| gptkbp:bfsParent |
gptkb:AS365_N2
gptkb:Aérospatiale_AS365N2_Dauphin |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Arriel 1C2
|