Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:certification |
gptkb:EASA
|
| gptkbp:compressor_type |
axial-centrifugal
|
| gptkbp:configuration |
single-spool
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:firstRun |
early 2000s
|
| gptkbp:fuelType |
gptkb:Jet-A1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Arriel 2C2
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:marketedAs |
gptkb:Safran_Helicopter_Engines
|
| gptkbp:part_of |
gptkb:Arriel_engine_family
|
| gptkbp:powerOutput |
up to 894 shp
|
| gptkbp:usedInAircraft |
gptkb:Eurocopter_EC145
gptkb:Airbus_Helicopters_H145 |
| gptkbp:bfsParent |
gptkb:Airbus_Helicopters_H155
|
| gptkbp:bfsLayer |
6
|