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gptkbp:instanceOf
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piston engine
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|
gptkbp:category
|
gptkb:Rolls-Royce_aircraft_engines
turbofan engines
military aircraft engines
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gptkbp:countryOfOrigin
|
gptkb:Germany
gptkb:Italy
gptkb:United_Kingdom
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gptkbp:developedBy
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gptkb:aircraft
|
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gptkbp:diameter
|
0.73 m
|
|
gptkbp:firstRun
|
1971
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce RB199
|
|
gptkbp:length
|
3.95 m
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
gptkb:MTU_Aero_Engines
gptkb:Avio
|
|
gptkbp:notableFeature
|
modular construction
compact design
reverse thrust capability
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|
gptkbp:numberOfAxles
|
3
|
|
gptkbp:numberOfStages
|
3
3 low-pressure, 5 high-pressure
|
|
gptkbp:relatedTo
|
gptkb:Rolls-Royce_Spey
Rolls-Royce EJ200
|
|
gptkbp:status
|
in service
|
|
gptkbp:thrust
|
40.5 kN
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:usedBy
|
gptkb:Royal_Air_Force
gptkb:Royal_Air_Force_of_Oman
gptkb:German_Air_Force
gptkb:Italian_Air_Force
gptkb:Royal_Saudi_Air_Force
|
|
gptkbp:usedInAircraft
|
gptkb:aircraft
BAe Sea Harrier (testbed)
|
|
gptkbp:weight
|
1035 kg
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_Defence
|
|
gptkbp:bfsLayer
|
7
|