|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:aircraft_operated
|
Bristol 188
|
|
gptkbp:application
|
gptkb:bomber
|
|
gptkbp:combustor_type
|
axial flow
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
hydraulic control
|
|
gptkbp:cooling_system
|
gptkb:water
air-cooled
|
|
gptkbp:design
|
gptkb:Bristol_Siddeley
|
|
gptkbp:development
|
gptkb:Bristol_Siddeley
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:Bristol_Siddeley_Orpheus
Brayton cycle
1,000 hours
air start
Bristol Siddeley family
|
|
gptkbp:engine_configuration
|
gptkb:1
pylon-mounted
single spool
|
|
gptkbp:engine_power
|
2,000 hours
|
|
gptkbp:engine_type
|
turbojet
BS.75 R
|
|
gptkbp:first_flight
|
gptkb:1958
|
|
gptkbp:fuel_economy
|
0.8 lb/hp/hr
|
|
gptkbp:fuel_type
|
kerosene
dual fuel system
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bristol Siddeley BS.75
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:length
|
14 ft 6 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Bristol_Siddeley
|
|
gptkbp:max_speed
|
Mach 2.0
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:number_of_stages
|
8
|
|
gptkbp:operational_range
|
1,500 miles
|
|
gptkbp:operational_use
|
gptkb:military_aircraft
|
|
gptkbp:propulsion
|
6.1
11,000 lbf
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_RB.168
|
|
gptkbp:turbine_type
|
axial turbine
|
|
gptkbp:type
|
afterburning turbojet
|
|
gptkbp:used_in
|
gptkb:Vulcan
|
|
gptkbp:weight
|
1,800 lb
|
|
gptkbp:bfsParent
|
gptkb:Vickers_VC10_family
|
|
gptkbp:bfsLayer
|
7
|