Rolls-Royce Pegasus

URI: https://gptkb.org/entity/Rolls-Royce_Pegasus

GPTKB entity

Predicate	Object
gptkbp:instanceOf	gptkb:piston_engine
gptkbp:category	gptkb: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
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
https://www.w3.org/2000/01/rdf-schema#label	Rolls-Royce Pegasus