Properties (53)
Predicate | Object |
---|---|
gptkbp:instanceOf |
turbofan engine
|
gptkbp:application |
military aircraft
civil aircraft |
gptkbp:controls |
hydromechanical control
|
gptkbp:coolingSystem |
air-cooled
|
gptkbp:diameter |
1.1 m
|
gptkbp:engine |
business jets
advanced technology drones experimental aircraft helicopters unmanned aerial vehicles military transport aircraft training aircraft high bypass ratio air start regional jets firefighting aircraft research aircraft agricultural aircraft aerial survey aircraft passenger aircraft aerial refueling aircraft search and rescue aircraft weather reconnaissance aircraft cargo_aircraft |
gptkbp:engineConfiguration |
twin-spool
|
gptkbp:enginePower |
7,500 to 10,000 lbf
|
gptkbp:engineType |
2
axial compressor axial turbine |
gptkbp:firstFlight |
1958
|
gptkbp:fuelType |
gptkb:Jet_A-1
|
https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Tyne
|
gptkbp:is_used_in |
gptkb:Vickers_VC10
de Havilland Comet 4 |
gptkbp:length |
3.4 m
|
gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
gptkbp:noise_level |
low noise
|
gptkbp:notableUsers |
gptkb:Boeing_707
gptkb:Lockheed_L-188_Electra gptkb:Boeing_737 gptkb:Boeing_720 |
gptkbp:number_of_stages |
8
|
gptkbp:operational_status |
1960s
|
gptkbp:performances |
modular design
high reliability high efficiency |
gptkbp:propulsion |
10,000 lbf
|
gptkbp:retirementYear |
1990s
|
gptkbp:successor |
gptkb:Rolls-Royce_RB.163
|
gptkbp:type |
turbojet engine
|
gptkbp:weight |
1,200 kg
|