Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
gptkb:Olympus
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
approximately 3 ft
|
| gptkbp:firstRun |
1946
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bristol Olympus engine
|
| gptkbp:laterDevelopedAs |
gptkb:Rolls-Royce/Snecma_Olympus_593
|
| gptkbp:length |
approximately 13 ft
|
| gptkbp:manufacturer |
gptkb:Bristol_Aeroplane_Company
|
| gptkbp:notableFor |
first two-spool axial-flow turbojet to enter service
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Rolls-Royce_Olympus
|
| gptkbp:thrust |
10,000 lbf (initial versions)
up to 20,000 lbf (later versions) |
| gptkbp:type |
axial-flow turbojet
|
| gptkbp:usedIn |
gptkb:aircraft
supersonic transport |
| gptkbp:usedInAircraft |
gptkb:aircraft
gptkb:BAC_TSR-2 gptkb:Handley_Page_Victor |
| gptkbp:bfsParent |
gptkb:Aerospace_Bristol
|
| gptkbp:bfsLayer |
6
|