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gptkbp:instanceOf
|
gptkb:piston_engine
|
|
gptkbp:category
|
afterburning jet engine
axial-flow turbofan
|
|
gptkbp:consortiumMembers
|
gptkb:Rolls-Royce
gptkb:MTU_Aero_Engines
gptkb:Avio_S.p.A.
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:developedBy
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gptkb:aircraft
|
|
gptkbp:diameter
|
0.72 m
|
|
gptkbp:firstFlight
|
1971
|
|
gptkbp:fuelType
|
aviation kerosene
|
|
gptkbp:introduced
|
1979
|
|
gptkbp:length
|
3.95 m
|
|
gptkbp:manufacturer
|
gptkb:Turbo-Union_Ltd.
|
|
gptkbp:notableFeature
|
modular construction
compact design
reverse thrust capability
|
|
gptkbp:numberBuilt
|
over 2,000
|
|
gptkbp:numberOfAxles
|
three
|
|
gptkbp:numberOfStages
|
three
three low-pressure, six high-pressure
|
|
gptkbp:operator
|
gptkb:Royal_Air_Force
gptkb:German_Air_Force
gptkb:Italian_Air_Force
gptkb:Royal_Saudi_Air_Force
|
|
gptkbp:primaryUse
|
gptkb:aircraft
|
|
gptkbp:relatedEngines
|
gptkb:Rolls-Royce_Spey
gptkb:Rolls-Royce_RB211
|
|
gptkbp:status
|
in service
|
|
gptkbp:thrust
|
40.5 kN
74.3 kN
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:usedInAircraft
|
gptkb:aircraft
|
|
gptkbp:weight
|
1,030 kg
|
|
gptkbp:bfsParent
|
gptkb:Tornado_GR4
|
|
gptkbp:bfsLayer
|
5
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbo-Union RB199
|