Statements (15)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
1.02 m
|
| gptkbp:firstFlight |
1950
|
| gptkbp:length |
4.42 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
gptkb:Bristol_Aero_Engines |
| gptkbp:notableFor |
first two-spool axial-flow turbojet engine
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
up to 38,000 lbf
|
| gptkbp:type |
turbojet
|
| gptkbp:usedIn |
gptkb:aircraft
|
| gptkbp:bfsParent |
gptkb:Bristol_Siddeley
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Olympus engine
|