Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
gptkb:Rolls-Royce_Pegasus
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:feature |
vectored thrust
short takeoff and vertical landing |
| gptkbp:firstFlight |
1959
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bristol Siddeley Pegasus
|
| gptkbp:introduced |
1966
|
| gptkbp:manufacturer |
gptkb:Bristol_Siddeley
gptkb:Rolls-Royce |
| gptkbp:notableFor |
enabling VTOL/STOVL flight
|
| gptkbp:numberBuilt |
over 1,200
|
| 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:usedInAircraft |
gptkb:Hawker_Siddeley_Harrier
gptkb:AV-8A_Harrier gptkb:AV-8B_Harrier_II gptkb:Sea_Harrier |
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Pegasus
|
| gptkbp:bfsLayer |
6
|