|
gptkbp:instanceOf
|
turbojet engine
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:controls
|
digital control system
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:developer
|
RB.199-34
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
low emissions
|
|
gptkbp:engine
|
gptkb:Royal_Air_Force
0.9 m
4.5 m
no
1,200 kg
axial compressor
single-stage turbine
annular combustion chamber
|
|
gptkbp:engineType
|
afterburning turbojet
axial compressor
single-stage turbine
RB.199-34R
|
|
gptkbp:firstFlight
|
1980
|
|
gptkbp:fuel_capacity
|
gptkb:Jet_A-1
high efficiency
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustion chamber
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce RB.199
|
|
gptkbp:is_used_in
|
Panavia Tornado
|
|
gptkbp:length
|
4.5 m
|
|
gptkbp:maintenance
|
2,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
advanced design features
|
|
gptkbp:notableUsers
|
gptkb:Royal_Air_Force
|
|
gptkbp:operationalRange
|
high-speed flight
|
|
gptkbp:performances
|
high efficiency
2,500 hours
|
|
gptkbp:propulsion
|
no
20,000 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:service_area
|
1982
|
|
gptkbp:serviceType
|
1982
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_EJ200
|
|
gptkbp:team
|
Rolls-Royce_engineers
|
|
gptkbp:type
|
afterburning turbojet
|
|
gptkbp:weight
|
1,200 kg
|