Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
V/STOL aircraft
|
| gptkbp:bypassRatio |
1.3:1
|
| gptkbp:compressionRatio |
two-spool axial
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
48 in
|
| gptkbp:family |
gptkb:Rolls-Royce_Pegasus
|
| gptkbp:firstFlight |
1980s
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Pegasus Mk 106
|
| gptkbp:length |
120 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableFeature |
vectored thrust
|
| gptkbp:thrust |
23,800 lbf
|
| gptkbp:usedBy |
gptkb:Royal_Air_Force
|
| gptkbp:usedIn |
gptkb:Harrier_GR9
|
| gptkbp:weight |
3,920 lb
|
| gptkbp:bfsParent |
gptkb:Sea_Harrier_FA2
|
| gptkbp:bfsLayer |
7
|