gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:aircraft_operated
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gptkb:Vulcan
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gptkbp:application
|
gptkb:military_aircraft
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gptkbp:combustor_type
|
axial flow
|
gptkbp:components
|
gptkb:turbofan_engine
gptkb:Noldor
gptkb:Control
gptkb:Blaster
gptkb:gasoline
gptkb:exhaust_system
mounting bracket
air intake
accessory gearbox
thrust reverser
starter motor
fuel control unit
|
gptkbp:compressor_type
|
8
|
gptkbp:control_system
|
hydraulic control
|
gptkbp:cooling_system
|
air-cooled
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
gptkbp:design
|
gptkb:Bristol_Siddeley
Bristol Siddeley engineers
|
gptkbp:development
|
5 years
|
gptkbp:diameter
|
3 ft 4 in
|
gptkbp:emissions_standard
|
gptkb:CAA
|
gptkbp:engine
|
gptkb:Bristol_Siddeley_Orpheus
Brayton cycle
|
gptkbp:engine_configuration
|
pylon-mounted
single spool
|
gptkbp:first_flight
|
gptkb:1958
|
gptkbp:fuel_economy
|
high
0.8 lb/lbf/hr
|
gptkbp:fuel_type
|
kerosene
|
gptkbp:historical_significance
|
pioneered military jet technology
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bristol Siddeley 505
|
gptkbp:ignition_system
|
spark ignition
|
gptkbp:introduced
|
gptkb:1958
|
gptkbp:involved_technology
|
jet propulsion
|
gptkbp:involved_units
|
gptkb:200
|
gptkbp:legacy
|
influenced future turbojet designs
|
gptkbp:length
|
12 ft 6 in
|
gptkbp:maintenance
|
100 hours
|
gptkbp:manufacturer
|
gptkb:Bristol_Siddeley
|
gptkbp:marketed_as
|
Bristol Siddeley 505 engine
|
gptkbp:max_speed
|
Mach 2.0
|
gptkbp:noise_level
|
85 d B
|
gptkbp:notable_feature
|
afterburner capability
|
gptkbp:operational_history
|
gptkb:Royal_Air_Force
|
gptkbp:operational_range
|
2000 miles
|
gptkbp:propulsion
|
4.17
5000 lbf
|
gptkbp:retired
|
1970s
|
gptkbp:service_ceiling
|
40,000 ft
|
gptkbp:successor
|
gptkb:Rolls-Royce_RB.168
|
gptkbp:turbine_type
|
2
|
gptkbp:type
|
afterburning turbojet
|
gptkbp:used_in
|
gptkb:Hawker_Siddeley_Buccaneer
|
gptkbp:weight
|
1200 lb
|
gptkbp:bfsParent
|
gptkb:Bristol_171_Sycamore
|
gptkbp:bfsLayer
|
7
|