|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
multirole fighter
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:compressionRatio
|
3.1
|
|
gptkbp:controls
|
digital
|
|
gptkbp:coolingSystem
|
air-cooled
advanced cooling techniques
|
|
gptkbp:customerService
|
gptkb:NATO
|
|
gptkbp:design_feature
|
high bypass ratio
|
|
gptkbp:developer
|
Eurojet Turbo GmbH
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
EASA_Chapter_4
|
|
gptkbp:engine
|
modular design
modular
|
|
gptkbp:engineConfiguration
|
ongoing
twin-spool
|
|
gptkbp:engineType
|
2
3
multiple configurations
afterburning turbofan
EJ200-30
|
|
gptkbp:exhaustSystem
|
variable geometry
|
|
gptkbp:firstFlight
|
1997
|
|
gptkbp:fuel_capacity
|
high
0.85 kg/kN/h
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
gptkbp:hasArea
|
extensive ground testing
EASA_certified
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce EJ200
|
|
gptkbp:is_used_in
|
Eurofighter Typhoon
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
3,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market
|
global support network
|
|
gptkbp:noise_level
|
low
advanced technology
|
|
gptkbp:notable_feature
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:operationalRange
|
high performance
up to 50,000 ft
|
|
gptkbp:performances
|
high
superior
meets military standards
over 4,000 hours
|
|
gptkbp:propulsion
|
7.5
optional
100 kN
90 kN
|
|
gptkbp:serviceType
|
2003
|
|
gptkbp:team
|
Rolls-Royce_and_MTU_Aero_Engines
|
|
gptkbp:updates
|
continuous development
|
|
gptkbp:weight
|
1,200 kg
|