Rolls-Royce Welland jet engine
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
gptkb:Rolls-Royce_RB.23
|
| gptkbp:combustionChambers |
10
|
| gptkbp:compressionRatio |
centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:developedBy |
Power Jets W.2B
|
| gptkbp:diameter |
41 in
|
| gptkbp:enteredService |
1943
|
| gptkbp:firstFlight |
1941
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Welland jet engine
|
| gptkbp:length |
100 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableFor |
first British jet engine to enter production
|
| gptkbp:predecessor |
gptkb:Power_Jets_W.2
|
| gptkbp:successor |
gptkb:Rolls-Royce_Derwent
|
| gptkbp:thrust |
1,600 lbf
|
| gptkbp:type |
turbojet
|
| gptkbp:usedDuring |
gptkb:World_War_II
|
| gptkbp:usedInAircraft |
gptkb:Gloster_Meteor
|
| gptkbp:weight |
850 lb
|
| gptkbp:bfsParent |
gptkb:Sir_Stanley_George_Hooker
|
| gptkbp:bfsLayer |
8
|