Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:combustionChambers |
7
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:designer |
gptkb:Frank_Whittle
|
| gptkbp:developedBy |
gptkb:Rolls-Royce_Welland
|
| gptkbp:diameter |
41 in
|
| gptkbp:firstFlight |
1943
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Derwent I
|
| gptkbp:length |
86 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:numberOfStages |
1
|
| gptkbp:status |
retired
|
| gptkbp:successor |
Rolls-Royce Derwent V
|
| gptkbp:thrust |
2,000 lbf
|
| gptkbp:type |
centrifugal-flow turbojet
|
| gptkbp:usedInAircraft |
gptkb:Gloster_Meteor
|
| gptkbp:weight |
1,150 lb
|
| gptkbp:bfsParent |
gptkb:Meteor_F.3
|
| gptkbp:bfsLayer |
6
|