|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Air_France_Flight_4590
gptkb:Rolls-Royce_Olympus_201
|
|
gptkbp:aircraft_operated
|
Concorde, Avro Vulcan
|
|
gptkbp:application
|
supersonic transport
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:controls
|
hydromechanical
digital control system.
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
10,000 hours
high performance.
Rolls-Royce engineers.
|
|
gptkbp:developer
|
gptkb:Rolls-Royce_Olympus_family
1950s to 1960s.
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:emissions_standard
|
variable geometry
mixed flow
ICAO Chapter 3
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_Olympus
gptkb:Rolls-Royce_Olympus_593_R
Brayton cycle
inline
air start
single spool
high efficiency.
high reliability.
excellent performance.
military and civilian use.
military and civilian aircraft.
powerful and efficient.
single spool.
|
|
gptkbp:engine_type
|
axial
turbojet.
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
0.5 lb/lbf/hr
0.6 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
annular
fuel injection.
|
|
gptkbp:historical_significance
|
first engine for Concorde.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Olympus 593
|
|
gptkbp:ignition_system
|
gptkb:park
|
|
gptkbp:inspiration
|
previous Rolls-Royce designs.
|
|
gptkbp:is_tested_for
|
extensive ground testing.
|
|
gptkbp:legacy
|
pioneering supersonic travel.
|
|
gptkbp:length
|
16 ft 6 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_achievement
|
first commercial supersonic airliner.
|
|
gptkbp:notable_features
|
afterburner
|
|
gptkbp:notable_users
|
gptkb:British_Airways
|
|
gptkbp:number_of_stages
|
2
8
|
|
gptkbp:operational_area
|
commercial aviation.
|
|
gptkbp:operational_history
|
used in military and civilian aircraft.
|
|
gptkbp:produced_by
|
over 1,000 units.
|
|
gptkbp:propulsion
|
22,000 lbf
14.67:1
|
|
gptkbp:retirement_year
|
gptkb:2003
|
|
gptkbp:services
|
gptkb:1969
|
|
gptkbp:successor
|
Rolls-Royce R B211
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:cape
|
|
gptkbp:water_source
|
3,000 lb/h
|
|
gptkbp:weight
|
1,500 lb
|