Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:developedBy |
gptkb:Rolls-Royce_Derwent
|
| gptkbp:diameter |
41 in
|
| gptkbp:firstFlight |
1943
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:length |
86 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:numberOfStages |
1
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
2,400 lbf
|
| gptkbp:type |
centrifugal-flow turbojet
|
| gptkbp:usedInAircraft |
gptkb:Gloster_Meteor
|
| gptkbp:weight |
1,250 lb
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Derwent
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Derwent V
|