Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:developedBy |
gptkb:Rolls-Royce_Derwent
|
| gptkbp:diameter |
41 in (1.04 m)
|
| gptkbp:engineType |
centrifugal-flow turbojet
|
| gptkbp:firstFlight |
1944
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Derwent Mk.IV
|
| gptkbp:length |
86 in (2.18 m)
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableFor |
used in the first jet-powered airliner flight (Avro Lancastrian)
|
| gptkbp:numberOfStages |
1
|
| gptkbp:relatedTo |
gptkb:Rolls-Royce_Welland
|
| gptkbp:successor |
gptkb:Rolls-Royce_Nene
|
| gptkbp:thrust |
2,400 lbf
|
| gptkbp:usedInAircraft |
gptkb:Gloster_Meteor
gptkb:Avro_Lancaster_(testbed) gptkb:FMA_I.Ae._27_Pulqui_I gptkb:Avro_Tudor_(testbed) |
| gptkbp:weight |
1,250 lb (567 kg)
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Derwent
|
| gptkbp:bfsLayer |
6
|