Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
low
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:designer |
gptkb:Bristol_Siddeley
|
| gptkbp:diameter |
0.88 m
|
| gptkbp:firstFlight |
1959
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pegasus engine
|
| gptkbp:length |
3.4 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:maximumSpeed |
97 kN
|
| gptkbp:notableFeature |
vectored thrust nozzles
|
| gptkbp:numberOfAxles |
two
|
| gptkbp:status |
in service
|
| gptkbp:thrustVectoring |
yes
|
| gptkbp:type |
turbofan
|
| gptkbp:usedIn |
gptkb:Harrier_Jump_Jet
gptkb:AV-8B_Harrier_II gptkb:Sea_Harrier Yakovlev Yak-38 (prototype only) |
| gptkbp:weight |
1,410 kg
|
| gptkbp:bfsParent |
gptkb:Bristol_Siddeley
|
| gptkbp:bfsLayer |
7
|