|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_Olympus_593
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:controls
|
digital control system
hydromechanical control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:date
|
gptkb:Monarch
|
|
gptkbp:developer
|
1940s to 1960s
|
|
gptkbp:engine
|
twin-spool
reliable operation
high thrust-to-weight ratio
high altitude performance
high speed performance
low specific fuel consumption
good acceleration
|
|
gptkbp:engine_type
|
axial compressor
single-stage turbine
|
|
gptkbp:first_flight
|
1950s
|
|
gptkbp:fuel_type
|
kerosene
annular combustion chamber
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Olympus family
|
|
gptkbp:innovation
|
high bypass ratio
afterburner
variable area nozzle
|
|
gptkbp:maintenance
|
modular design
field-replaceable units
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:notable_users
|
gptkb:aircraft
gptkb:British_Airways
gptkb:NASA
gptkb:military_base
|
|
gptkbp:operational_area
|
supersonic flight
subsonic flight
|
|
gptkbp:propulsion
|
up to 30,000 lbf
|
|
gptkbp:range
|
15,000 to 30,000 lbf
|
|
gptkbp:retirement_year
|
gptkb:2003
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_Trent
Rolls-Royce R B211
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Lockheed_SR-71_Blackbird
gptkb:cape
gptkb:military_officer
|
|
gptkbp:variant
|
gptkb:Olympus_301
gptkb:Olympus_722
Olympus 593
|
|
gptkbp:weight
|
approximately 3,000 lb
|