Bristol Siddeley BS.605

GPTKB entity

Statements (53)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:aircraft_operated gptkb:Vulcan
gptkbp:certification certified by UK authorities
gptkbp:combustor_type axial flow
gptkbp:compressor_type axial compressor
gptkbp:control_system hydromechanical control system
gptkbp:cooling_system air-cooled
gptkbp:country_of_origin gptkb:United_Kingdom
gptkbp:design gptkb:Bristol_Siddeley
gptkbp:diameter 3 ft 4 in
gptkbp:engine gptkb:Bristol_Siddeley_BS.605_R
Brayton cycle
influenced future designs
various military applications
produced in limited numbers
used in various military aircraft models
developed during the Cold War
notable features include high thrust
part of British aviation history
production ceased in the 1970s
utilizes advanced technology for its time
gptkbp:engine_configuration detailed specifications available
single spool
low bypass ratio
characteristics include compact design
specifications include thrust and dimensions
gptkbp:engine_power reliable engine
high thrust-to-weight ratio
moderate thermal efficiency
performance metrics include speed and altitude
gptkbp:engine_type multiple variants developed
BS.605 R
gptkbp:first_flight gptkb:1958
gptkbp:fuel_type kerosene
https://www.w3.org/2000/01/rdf-schema#label Bristol Siddeley BS.605
gptkbp:impact had significant impact on jet engine design.
gptkbp:introduced gptkb:1958
gptkbp:is_tested_for extensively tested
gptkbp:length 12 ft 6 in
gptkbp:maintenance moderate maintenance requirements
gptkbp:manufacturer gptkb:Bristol_Siddeley
gptkbp:noise_level high noise level
gptkbp:notable_users gptkb:Royal_Air_Force
gptkbp:operational_history used in military aircraft
gptkbp:propulsion 6000 lbf
gptkbp:retired 1970s
gptkbp:successor gptkb:Rolls-Royce_RB.162
gptkbp:turbine_type single stage turbine
gptkbp:type gptkb:turbofan_engine
gptkbp:used_in gptkb:Hawker_Siddeley_Buccaneer
gptkbp:weight 1200 lb
gptkbp:bfsParent gptkb:Vickers_VC10
gptkbp:bfsLayer 5