|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:category
|
afterburning turbofan
military aircraft engine
|
|
gptkbp:combustorType
|
annular combustor
|
|
gptkbp:compressionRatio
|
3-stage fan
5-stage low-pressure compressor
single-stage high-pressure compressor
|
|
gptkbp:countryOfOrigin
|
gptkb:Germany
gptkb:Italy
gptkb:Spain
gptkb:United_Kingdom
|
|
gptkbp:developedBy
|
gptkb:Rolls-Royce
gptkb:Avio_Aero
gptkb:MTU_Aero_Engines
gptkb:Industria_de_Turbo_Propulsores
|
|
gptkbp:diameter
|
0.737 m
|
|
gptkbp:enteredService
|
2003
|
|
gptkbp:firstFlight
|
1998
|
|
gptkbp:fuelType
|
aviation kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Eurojet EJ200
|
|
gptkbp:intendedAircraft
|
gptkb:Eurofighter_Typhoon
|
|
gptkbp:length
|
4.0 m
|
|
gptkbp:manufacturer
|
gptkb:EuroJet_Turbo_GmbH
|
|
gptkbp:notableFeature
|
modular design
high thrust-to-weight ratio
supercruise capability
low maintenance requirements
digital engine control
|
|
gptkbp:numberOfAxles
|
2
|
|
gptkbp:relatedTo
|
Eurofighter program
Rolls-Royce XG-40
|
|
gptkbp:status
|
in production
|
|
gptkbp:thrust
|
60 kN
90 kN
|
|
gptkbp:turbineType
|
single-stage high-pressure turbine
single-stage low-pressure turbine
|
|
gptkbp:usedBy
|
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:usedIn
|
gptkb:Eurofighter_Typhoon
|
|
gptkbp:weight
|
989 kg
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_RB.199
gptkb:Qatar_Emiri_Air_Force_Eurofighter_Typhoon
gptkb:Eurofighter_Typhoon_engines
gptkb:Austrian_Eurofighter_Typhoon
|
|
gptkbp:bfsLayer
|
7
|