|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:bypassRatio
|
0.4:1
|
|
gptkbp:controls
|
Full Authority Digital Engine Control (FADEC)
|
|
gptkbp:countryOfOrigin
|
gptkb:Germany
gptkb:Italy
gptkb:Spain
gptkb:United_Kingdom
|
|
gptkbp:developedBy
|
gptkb:Eurofighter_Typhoon
|
|
gptkbp:diameter
|
0.737 m
|
|
gptkbp:firstFlight
|
1995
|
|
gptkbp:fuelType
|
aviation kerosene
|
|
gptkbp:hasConcept
|
axial flow
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
EJ200 turbofan engine
|
|
gptkbp:introduced
|
2003
|
|
gptkbp:length
|
4.0 m
|
|
gptkbp:manufacturer
|
gptkb:EuroJet_Turbo_GmbH
|
|
gptkbp:maximumSpeed
|
15,000 rpm
|
|
gptkbp:notableFeature
|
modular design
high thrust-to-weight ratio
low maintenance requirements
growth potential for higher thrust variants
|
|
gptkbp:numberOfAxles
|
2
|
|
gptkbp:numberOfStages
|
1 high-pressure, 1 low-pressure
3 low-pressure, 5 high-pressure
|
|
gptkbp:operator
|
gptkb:Qatar_Emiri_Air_Force
gptkb:Royal_Air_Force
gptkb:Oman_Air_Force
gptkb:German_Air_Force
gptkb:Italian_Air_Force
gptkb:Austrian_Air_Force
gptkb:Royal_Saudi_Air_Force
gptkb:Spanish_Air_Force
gptkb:Kuwait_Air_Force
|
|
gptkbp:relatedTo
|
RB199
|
|
gptkbp:status
|
in production
|
|
gptkbp:thrust
|
yes
60 kN
90 kN
|
|
gptkbp:thrustToWeightRatio
|
9:1
|
|
gptkbp:usedIn
|
gptkb:Eurofighter_Typhoon
|
|
gptkbp:weight
|
989 kg
|
|
gptkbp:bfsParent
|
gptkb:Eurojet_Turbo_GmbH
|
|
gptkbp:bfsLayer
|
7
|