Harrier jump jet engine (Pegasus)
GPTKB entity
Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
gptkb:Rolls-Royce_Pegasus
|
| gptkbp:bypassRatio |
1.3:1
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:designer |
gptkb:Gordon_Lewis
gptkb:Sir_Stanley_Hooker |
| gptkbp:diameter |
48 in (1.22 m)
|
| gptkbp:firstFlight |
1960
|
| gptkbp:firstRun |
1959
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Harrier jump jet engine (Pegasus)
|
| gptkbp:length |
120 in (3.05 m)
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableFeature |
vectored thrust nozzles
|
| gptkbp:notableUser |
gptkb:Royal_Air_Force
gptkb:United_States_Marine_Corps |
| gptkbp:numberOfStages |
2
8 |
| gptkbp:status |
in service
|
| gptkbp:thrust |
21,750 lbf (Pegasus 11-61)
|
| gptkbp:type |
two-shaft turbofan
|
| gptkbp:usedFor |
VTOL/STOL aircraft
|
| gptkbp:usedIn |
gptkb:Hawker_Siddeley_Harrier
gptkb:AV-8A_Harrier gptkb:AV-8B_Harrier_II gptkb:Sea_Harrier |
| gptkbp:weight |
3,920 lb (1,780 kg)
|
| gptkbp:bfsParent |
gptkb:Sir_Stanley_Hooker
|
| gptkbp:bfsLayer |
6
|