Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
gptkb:Bristol_Siddeley_Pegasus
gptkb:Rolls-Royce_Pegasus |
| gptkbp:bypassRatio |
low
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:developedBy |
gptkb:Orpheus_engine
|
| gptkbp:diameter |
0.88 m
|
| gptkbp:firstFlight |
1960
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pegasus turbofan
|
| gptkbp:length |
3.3 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:maximumSpeed |
97 kN
|
| gptkbp:notableFeature |
vectored thrust nozzles
vertical/short takeoff capability |
| gptkbp:numberOfAxles |
two
|
| gptkbp:numberOfStages |
2
8 |
| gptkbp:primaryUser |
gptkb:Royal_Air_Force
gptkb:United_States_Marine_Corps |
| gptkbp:thrustVectoring |
yes
|
| gptkbp:type |
turbofan
|
| gptkbp:usedFor |
gptkb:helicopter
|
| gptkbp:usedIn |
gptkb:Harrier_Jump_Jet
gptkb:AV-8B_Harrier_II |
| gptkbp:weight |
1,410 kg
|
| gptkbp:bfsParent |
gptkb:Hawker_Siddeley_Harrier_GR.3
gptkb:Hawker_Siddeley_Harrier gptkb:AV-8A_Harrier gptkb:Harrier_GR3 |
| gptkbp:bfsLayer |
6
|