Rolls-Royce Pegasus

URI: https://gptkb.org/entity/Rolls-Royce_Pegasus
GPTKB entity
Statements (30)
Predicate Object
gptkbp:instanceOf piston engine
gptkbp:category piston engine
gptkbp:compressionRatio two-spool axial
gptkbp:countryOfOrigin gptkb:United_Kingdom
gptkbp:developedBy gptkb:Bristol_Siddeley
gptkbp:diameter 0.88 m
gptkbp:enteredService 1969
gptkbp:feature vectored thrust
gptkbp:firstFlight 1959
https://www.w3.org/2000/01/rdf-schema#label Rolls-Royce Pegasus
gptkbp:length 3.3 m
gptkbp:manufacturer gptkb:Rolls-Royce
gptkbp:notableFor enabling vertical/short takeoff and landing
gptkbp:numberOfAxles two
gptkbp:originalName gptkb:Bristol_Siddeley_Pegasus
gptkbp:primaryUse gptkb:helicopter
gptkbp:producedBy gptkb:Rolls-Royce
gptkbp:status in service
gptkbp:successor gptkb:Rolls-Royce_F402
gptkbp:thrust up to 23,800 lbf
gptkbp:type turbofan
gptkbp:usedBy gptkb:Royal_Air_Force
gptkb:Royal_Navy
gptkb:United_States_Marine_Corps
gptkbp:usedIn gptkb:Harrier_Jump_Jet
gptkb:AV-8B_Harrier_II
gptkb:Sea_Harrier
gptkbp:weight 1,410 kg
gptkbp:bfsParent gptkb:Harrier_Jump_Jet
gptkbp:bfsLayer 5