Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:configuration |
free-turbine
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
2 ft 10 in (0.86 m)
|
| gptkbp:firstRun |
1947
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Proteus engine
|
| gptkbp:length |
12 ft 2 in (3.71 m)
|
| gptkbp:manufacturer |
gptkb:Bristol_Aeroplane_Company
|
| gptkbp:notableFeature |
reverse-flow combustion chambers
axial compressor |
| gptkbp:numberOfStages |
2
12 |
| gptkbp:powerOutput |
3,780 shp
|
| gptkbp:status |
retired
|
| gptkbp:type |
turboprop
|
| gptkbp:usedIn |
gptkb:Bristol_Britannia
gptkb:Saunders-Roe_Princess Bristol Brabazon Mk.II |
| gptkbp:weight |
2,800 lb (1,270 kg)
|
| gptkbp:bfsParent |
gptkb:Bristol_Siddeley
|
| gptkbp:bfsLayer |
7
|