Turbomeca Arrius 2B2

URI: https://gptkb.org/entity/Turbomeca_Arrius_2B2
GPTKB entity
Statements (20)
Predicate Object
gptkbp:instanceOf gptkb: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
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 7
https://www.w3.org/2000/01/rdf-schema#label Turbomeca Arrius 2B2