|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:alsoKnownAs
|
gptkb:Bristol_Olympus
|
|
gptkbp:compressor_type
|
axial flow
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:designer
|
gptkb:Bristol_Aero_Engines
|
|
gptkbp:diameter
|
40 in (1.02 m)
|
|
gptkbp:firstFlight
|
1952
|
|
gptkbp:firstRun
|
1950
|
|
gptkbp:fuelType
|
aviation kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Olympus
|
|
gptkbp:length
|
154 in (3.91 m)
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:notable_for
|
long service life
marine gas turbine applications
supersonic flight capability (in Concorde)
|
|
gptkbp:notableFeature
|
first two-spool axial-flow turbojet engine
|
|
gptkbp:notableVariant
|
gptkb:Olympus_593
|
|
gptkbp:numberOfStages
|
2
14
|
|
gptkbp:Olympus_101_used_in
|
gptkb:aircraft
|
|
gptkbp:Olympus_102_used_in
|
gptkb:aircraft
|
|
gptkbp:Olympus_104_used_in
|
gptkb:aircraft
|
|
gptkbp:Olympus_111_used_in
|
gptkb:aircraft
|
|
gptkbp:Olympus_201_used_in
|
gptkb:BAC_TSR-2
|
|
gptkbp:Olympus_301_used_in
|
gptkb:aircraft
|
|
gptkbp:Olympus_320_used_in
|
gptkb:aircraft
|
|
gptkbp:Olympus_593_used_in
|
gptkb:aircraft
|
|
gptkbp:predecessor
|
gptkb:Bristol_Theseus
|
|
gptkbp:retired_from_Concorde
|
2003
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_RB211
|
|
gptkbp:thrust_range
|
11,000 lbf to 38,000 lbf
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:used_in
|
gptkb:ship
gptkb:Type_82_destroyer
power generation
Royal Navy ships
industrial applications
Invincible-class aircraft carrier
marine applications
gas pipeline compressors
|
|
gptkbp:usedInAircraft
|
gptkb:aircraft
gptkb:Bristol_Britannia_(prototype)
gptkb:BAC_TSR-2
|
|
gptkbp:weight
|
3,320 lb (1,506 kg)
|
|
gptkbp:bfsParent
|
gptkb:Bristol_Olympus
gptkb:Rolls-Royce_Limited
gptkb:The_Spirit_of_Great_Britain
|
|
gptkbp:bfsLayer
|
6
|