Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:alsoKnownAs |
gptkb:Pegasus
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:category |
military aircraft engine
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
two-stage fan, eight-stage LP compressor, two-stage HP compressor
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:developedBy |
gptkb:Bristol_Siddeley_Pegasus
|
| gptkbp:diameter |
48 inches
|
| gptkbp:firstFlight |
1966
|
| gptkbp:hasTower |
two-stage HP, two-stage LP
|
| gptkbp:introduced |
1970s
|
| gptkbp:length |
146 inches
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableFeature |
vectored thrust
|
| gptkbp:primaryUser |
gptkb:Royal_Air_Force
gptkb:United_States_Marine_Corps |
| gptkbp:relatedTo |
gptkb:Bristol_Pegasus
|
| gptkbp:thrust |
23,800 lbf
|
| gptkbp:type |
turbofan
|
| gptkbp:usedIn |
gptkb:AV-8B_Harrier_II
gptkb:Sea_Harrier gptkb:Harrier_GR5 |
| gptkbp:weight |
3,920 lb
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Pegasus
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce F402
|