Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
supersonic transport
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:developedBy |
gptkb:Bristol_Olympus
|
| gptkbp:diameter |
1.02 m (3 ft 4 in)
|
| gptkbp:firstFlight |
1966
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:length |
4.43 m (14 ft 6 in)
|
| gptkbp:manufacturer |
gptkb:Snecma
gptkb:Rolls-Royce_Limited |
| gptkbp:notableFeature |
designed for sustained supersonic flight
afterburner equipped |
| gptkbp:numberOfStages |
2
14 |
| gptkbp:retired |
2003
|
| gptkbp:thrust |
38,000 lbf (170 kN)
|
| gptkbp:type |
afterburning turbojet
|
| gptkbp:usedBy |
gptkb:Air_France
gptkb:British_Airways |
| gptkbp:usedIn |
gptkb:aircraft
|
| gptkbp:weight |
3,820 kg (8,422 lb)
|
| gptkbp:bfsParent |
gptkb:Bristol_Olympus
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Olympus 593
|