Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:developedBy |
de Havilland Engine Company design
|
| gptkbp:diameter |
0.39 m
|
| gptkbp:firstFlight |
1967
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:length |
1.3 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:marketedAs |
gptkb:Rolls-Royce_plc
|
| gptkbp:notableFor |
used in Lynx helicopter world speed record
|
| gptkbp:numberOfAxles |
three
|
| gptkbp:powerOutput |
1120 shp
|
| gptkbp:primaryUser |
gptkb:Royal_Navy
|
| gptkbp:status |
in service
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:Westland_Lynx
|
| gptkbp:weight |
170 kg
|
| gptkbp:bfsParent |
gptkb:Westland_Lynx
|
| gptkbp:bfsLayer |
6
|
| http://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Gem
|