Olympus 104
E870903
Olympus 104 is a specific variant of the Rolls-Royce Olympus turbojet engine, developed for improved performance in military and aviation applications.
All labels observed (1)
| Label | Occurrences |
|---|---|
| Olympus 104 canonical | 1 |
Statements (25)
| Predicate | Object |
|---|---|
| instanceOf |
Rolls-Royce Olympus variant
ⓘ
turbojet engine variant ⓘ |
| applicationDomain | aircraft propulsion ⓘ |
| combustionSystem | annular combustor ⓘ |
| compressorType | axial-flow compressor ⓘ |
| configuration | single-spool turbojet ⓘ |
| coolingMethod | air-cooled turbine ⓘ |
| countryOfOrigin | United Kingdom ⓘ |
| designFocus |
high thrust-to-weight ratio
ⓘ
reliability in military service ⓘ |
| designGoal | improved performance ⓘ |
| developedBy | Rolls-Royce Limited NERFINISHED ⓘ |
| engineType | turbojet ⓘ |
| era | Cold War period NERFINISHED ⓘ |
| familyRole | intermediate development mark in Olympus series ⓘ |
| fuelType | kerosene-based aviation fuel ⓘ |
| hasFeature | afterburner-capable in some installations ⓘ |
| improvementOver | earlier Rolls-Royce Olympus marks ⓘ |
| intendedUse | military aviation ⓘ |
| manufacturer | Rolls-Royce NERFINISHED ⓘ |
| originatesFrom | Bristol Olympus design lineage ⓘ |
| partOfEngineFamily | Rolls-Royce Olympus NERFINISHED ⓘ |
| thrustClass | medium-to-high thrust military turbojet ⓘ |
| usedFor | high-speed aircraft ⓘ |
| usedIn | military aircraft ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.
subject surface form:
Rolls-Royce Olympus