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 2

How this entity was disambiguated

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 ⓘ
engineType turbojet ⓘ
era Cold War period ⓘ
linked to: Cold War
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 ⓘ
linked to: Rolls-Royce plc
originatesFrom Bristol Olympus design lineage ⓘ
partOfEngineFamily Rolls-Royce Olympus ⓘ
thrustClass medium-to-high thrust military turbojet ⓘ
usedFor high-speed aircraft ⓘ
usedIn military aircraft ⓘ

How these facts were elicited

Referenced by (2)

Full triples — surface form annotated when it differs from this entity's canonical label.

Rolls-Royce Olympus → notableVariant → Olympus 104 ⓘ
subject linked to: Rolls-Royce Olympus turbojet
Olympus 101 → successor → Olympus 104 ⓘ