Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:designer |
gptkb:Sir_Stanley_Hooker
|
| gptkbp:enteredService |
1950
|
| gptkbp:firstRun |
1946
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bristol Olympus
|
| gptkbp:laterDevelopedAs |
gptkb:Rolls-Royce_Olympus
|
| gptkbp:manufacturer |
gptkb:Bristol_Aero_Engines
|
| gptkbp:notableFor |
first two-spool axial-flow turbojet engine
|
| gptkbp:numberOfStages |
2
14 |
| gptkbp:successor |
gptkb:Rolls-Royce_Olympus_593
|
| gptkbp:thrust |
10,000 lbf (early versions)
20,000 lbf (Concorde version) |
| gptkbp:type |
axial-flow turbojet
|
| gptkbp:usedInAircraft |
gptkb:aircraft
gptkb:BAC_TSR-2 gptkb:Handley_Page_Victor |
| gptkbp:usedInBomber |
gptkb:aircraft
|
| gptkbp:usedInSupersonicTransport |
gptkb:aircraft
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce/Snecma_Olympus_593_turbojet
|
| gptkbp:bfsLayer |
5
|