Rolls-Royce Olympus 201

URI: https://gptkb.org/entity/Rolls-Royce_Olympus_201
GPTKB entity
Statements (56)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:bfsLayer 4
gptkbp:bfsParent gptkb:Avro_Vulcan_K.2
gptkbp:aircraft_operated gptkb:military_officer
gptkbp:compression_ratio 22:1
gptkbp:controls hydromechanical
gptkbp:cooling_system air-cooled
gptkbp:date gptkb:Monarch
gptkbp:diameter 3 ft 4 in
gptkbp:engine gptkb:4
gptkb:Rolls-Royce_Olympus_593
high
advanced aerodynamics
commercial aviation
excellent
supersonic transport
Brayton cycle
axial-flow
high bypass ratio
pioneering turbojet technology
Rolls-Royce design philosophy
gptkbp:engine_type high-pressure turbine
gptkbp:fan_art single-spool
gptkbp:first_flight gptkb:1969
gptkbp:fuel_capacity high
0.8 lb/hp·h
gptkbp:fuel_type annular
kerosene
https://www.w3.org/2000/01/rdf-schema#label Rolls-Royce Olympus 201
gptkbp:ignition_system gptkb:park
gptkbp:impact gptkb:aircraft
gptkbp:introduced 1960s
gptkbp:length 16 ft 6 in
15 ft 6 in
gptkbp:maintenance moderate
gptkbp:manufacturer gptkb:Rolls-Royce
gptkbp:noise_level low
gptkbp:notable_users gptkb:British_Airways
gptkbp:number_of_stages 8
gptkbp:operational_area gptkb:aircraft
gptkbp:origin gptkb:United_Kingdom
gptkbp:original_run gptkb:1958
gptkbp:propulsion 22,000 lbf
14.67:1
gptkbp:related_to gptkb:Rolls-Royce_Olympus_593
gptkbp:retired gptkb:2003
gptkbp:retirement_year gptkb:2003
gptkbp:services gptkb:1960
gptkbp:serving_temperature 1,600 ° F
gptkbp:successor Rolls-Royce R B211
gptkbp:supports 60 lb/s
gptkbp:type gptkb:engine
turbojet
gptkbp:used_in gptkb:cape
gptkbp:variant Olympus 593
gptkbp:weight 1,500 lb