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Rolls-Royce Pegasus turbofan
URI:
https://gptkb.org/entity/Rolls-Royce_Pegasus_turbofan
GPTKB entity
Statements (35)
Predicate
Object
gptkbp:instanceOf
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
https://www.w3.org/2000/01/rdf-schema#label
Rolls-Royce Pegasus turbofan
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_GR9
gptkb:AV-8B_Harrier_II_Plus
gptkb:Harrier_GR7
gptkb:Sea_Harrier_FRS1
gptkbp:bfsLayer
7