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gptkbp:instance_of
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gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Folland_Gnat
gptkb:Hawker_Hunter
gptkb:BAC_Lightning
gptkb:de_Havilland_Sea_Vixen
Bristol 188
|
|
gptkbp:average_temperature
|
1,000 ° C
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
hydraulic
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:development
|
gptkb:Bristol_Siddeley_Orpheus_702
gptkb:Bristol_Siddeley_Orpheus_704
Bristol Siddeley Orpheus 700
Bristol Siddeley Orpheus 701
Bristol Siddeley Orpheus 708
Bristol Siddeley Orpheus 709
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:emissions_standard
|
gptkb:CAA
|
|
gptkbp:engine
|
gptkb:Bristol_Orpheus
gptkb:Bristol_Siddeley_Orpheus_703
Brayton cycle
air start
Bristol Siddeley Orpheus 706
Bristol Siddeley Orpheus 707
|
|
gptkbp:engine_configuration
|
rear-mounted
single spool
|
|
gptkbp:first_flight
|
gptkb:1958
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
0.8 lb/hp/hr
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bristol Siddeley Orpheus 705
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:introduced
|
gptkb:1958
|
|
gptkbp:length
|
14 ft 6 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Bristol_Siddeley
|
|
gptkbp:max_speed
|
Mach 2.0
|
|
gptkbp:noise_level
|
0.5 g
85 d B
|
|
gptkbp:operational_range
|
1,000 miles
|
|
gptkbp:operational_use
|
gptkb:military_aircraft
|
|
gptkbp:propulsion
|
4.67
7000 lbf
|
|
gptkbp:retired
|
gptkb:1980s
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_RB.168
gptkb:Rolls-Royce_Spey
|
|
gptkbp:turbine_type
|
single stage
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:used_in
|
gptkb:Hawker_Siddeley_Buccaneer
|
|
gptkbp:weight
|
1,500 lb
|