Rolls-Royce Pegasus turbofan

GPTKB entity

Predicate	Object
gptkbp:instanceOf	gptkb:piston_engine
gptkbp:bypassRatio	low
gptkbp:countryOfOrigin	gptkb:United_Kingdom
gptkbp:designer	gptkb:Bristol_Siddeley
gptkbp:developedBy	gptkb:Bristol_Siddeley_Orpheus
gptkbp:diameter	approximately 0.88 m
gptkbp:enteredService	1969
gptkbp:firstFlight	1959
gptkbp:fuelType	aviation kerosene
gptkbp:hasNozzle	4 vectoring nozzles
gptkbp:length	approximately 3.3 m
gptkbp:mainActivity	gptkb:helicopter
gptkbp:manufacturer	gptkb:Rolls-Royce
gptkbp:maximumSpeed	up to 23,800 lbf
gptkbp:militaryDesignation	F402 (US)
gptkbp:notableFeature	vertical/short takeoff and landing (V/STOL) capability
gptkbp:notableUser	gptkb:Royal_Air_Force gptkb:United_States_Marine_Corps
gptkbp:numberOfAxles	two
gptkbp:numberOfStages	2 8
gptkbp:status	in service
gptkbp:thrustVectoring	yes
gptkbp:type	turbofan
gptkbp:usedIn	gptkb:Harrier_Jump_Jet gptkb:AV-8B_Harrier_II gptkb:Sea_Harrier
gptkbp:weight	approximately 1,400 kg
gptkbp:bfsParent	gptkb:Sea_Harrier_jet gptkb:Harrier_GR7 gptkb:Sea_Harrier_FRS1
gptkbp:bfsLayer	7
https://www.w3.org/2000/01/rdf-schema#label	Rolls-Royce Pegasus turbofan