Bristol Siddeley Proteus

GPTKB entity

Properties (46)
Predicate Object
gptkbp:instanceOf turboprop engine
gptkbp:application military aviation
civil aviation
gptkbp:controls hydromechanical
gptkbp:coolingSystem air-cooled
gptkbp:design gptkb:Bristol_Aeroplane_Company
gptkbp:developer gptkb:Bristol_Siddeley
gptkbp:diameter 2.5 ft
gptkbp:emissionsStandard low emissions
gptkbp:engineType turboprop
axial
free turbine
gptkbp:firstFlight 1953
gptkbp:fuel_capacity 0.5 lb/hp/hr
gptkbp:fuelType annular
spark ignition
kerosene
https://www.w3.org/2000/01/rdf-schema#label Bristol Siddeley Proteus
gptkbp:is_used_in gptkb:Bristol_Britannia
Vickers Viscount
gptkbp:landing_gear planetary gear
gptkbp:legacy influenced future turboprop designs
gptkbp:length 4.5 ft
gptkbp:maintenance 1,000 hours
gptkbp:manufacturer gptkb:Bristol_Siddeley
gptkbp:market commercial aviation
military aviation
gptkbp:noise_level low noise
gptkbp:notableUsers gptkb:Trans-Canada_Air_Lines
gptkb:Royal_Air_Force
gptkb:Royal_Canadian_Air_Force
gptkb:Aero_Spacelines
gptkb:British_Overseas_Airways_Corporation
gptkbp:number_of_stages 6 stages
gptkbp:operationalHistory 1953 to 1980s
gptkbp:operationalRange up to 25,000 ft
gptkbp:patentCitation several patents filed
gptkbp:performances detailed technical specifications available.
gptkbp:powerOutput 1,500 hp
gptkbp:propulsion 1,500 to 2,000 lbf
gptkbp:related_engine Brayton_cycle
gptkbp:research extensive research and development
gptkbp:retirementYear 1980s
gptkbp:setting two-shaft
gptkbp:successor gptkb:Rolls-Royce_Tyne
gptkbp:weight 1,200 lb