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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:aircraft_operated
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gptkb:De_Havilland_Sea_Vixen
gptkb:Folland_Gnat
gptkb:Hawker_Hunter
gptkb:BAC_Strikemaster
gptkb:de_Havilland_Sea_Vixen
Bristol 188
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gptkbp:combustor_type
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axial flow
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gptkbp:compressor_type
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8
axial compressor
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gptkbp:control_system
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hydraulic control
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gptkbp:cooling_system
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air-cooled
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gptkbp:design
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gptkb:Bristol_Siddeley_Orpheus_family
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gptkbp:design_purpose
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gptkb:aircraft
gptkb:military_aircraft
gptkb:trainer_aircraft
gptkb:fighter_aircraft
civil aircraft
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gptkbp:development
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gptkb:Bristol_Siddeley_Orpheus_702
gptkb:Bristol_Siddeley_Orpheus_704
gptkb:Bristol_Siddeley_Orpheus_705
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gptkbp:diameter
|
0.9 m
3 ft 4 in
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gptkbp:engine
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gptkb:Bristol_Siddeley_Orpheus_703_AA
gptkb:Bristol_Siddeley_Orpheus_703_AB
gptkb:Bristol_Siddeley_Orpheus_703_AC
gptkb:Bristol_Siddeley_Orpheus_703_AD
gptkb:Bristol_Siddeley_Orpheus_703_AE
gptkb:Bristol_Siddeley_Orpheus_703_AF
gptkb:Bristol_Siddeley_Orpheus_703_AG
gptkb:Bristol_Siddeley_Orpheus_703_AH
gptkb:Bristol_Siddeley_Orpheus_703_AI
gptkb:Bristol_Siddeley_Orpheus_703_AJ
gptkb:Bristol_Siddeley_Orpheus_703_AK
gptkb:Bristol_Siddeley_Orpheus_703_AL
gptkb:Bristol_Siddeley_Orpheus_703_AM
gptkb:Bristol_Siddeley_Orpheus_703_AN
gptkb:Bristol_Siddeley_Orpheus_703_AO
gptkb:Bristol_Siddeley_Orpheus_703_AP
gptkb:Bristol_Siddeley_Orpheus_703_AQ
gptkb:Bristol_Siddeley_Orpheus_703_AR
gptkb:Bristol_Siddeley_Orpheus_703_AS
gptkb:Bristol_Siddeley_Orpheus_703_AT
gptkb:Bristol_Siddeley_Orpheus_703_AU
gptkb:Bristol_Siddeley_Orpheus_703_AV
gptkb:Bristol_Siddeley_Orpheus_703_AW
gptkb:Bristol_Siddeley_Orpheus_703_AX
gptkb:Bristol_Siddeley_Orpheus_703_AY
gptkb:Bristol_Siddeley_Orpheus_703_AZ
gptkb:Bristol_Siddeley_Orpheus_703_R
gptkb:Bristol_Siddeley_Orpheus_703_S
gptkb:Bristol_Siddeley_Orpheus_703_T
gptkb:Bristol_Siddeley_Orpheus_703_U
gptkb:Bristol_Siddeley_Orpheus_703_V
gptkb:Bristol_Siddeley_Orpheus_703_W
gptkb:Bristol_Siddeley_Orpheus_703_X
gptkb:Bristol_Siddeley_Orpheus_703_Y
gptkb:Bristol_Siddeley_Orpheus_703_Z
Brayton cycle
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gptkbp:engine_configuration
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single spool
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gptkbp:exhaust_system
|
straight exhaust
|
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gptkbp:first_flight
|
gptkb:1958
|
|
gptkbp:fuel_economy
|
0.8 lb/hp/hr
0.6 lb/lbf/hr
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gptkbp:fuel_type
|
kerosene
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Bristol Siddeley Orpheus 703
|
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gptkbp:ignition_system
|
spark ignition
|
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gptkbp:introduced
|
gptkb:1958
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|
gptkbp:length
|
3.4 m
12 ft 6 in
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gptkbp:manufacturer
|
gptkb:Bristol_Siddeley
|
|
gptkbp:notable_feature
|
high thrust-to-weight ratio
afterburner
variable area nozzle
reheat capability
|
|
gptkbp:operational_history
|
gptkb:Royal_Air_Force
gptkb:Royal_Navy
used by Indian Air Force
used by Royal Air Force
used by Royal Australian Air Force
used by Royal Navy
used by South African Air Force
|
|
gptkbp:operational_range
|
high altitude
subsonic speeds
|
|
gptkbp:propulsion
|
5,000 lbf
22 k N
|
|
gptkbp:replaced_by
|
gptkb:Rolls-Royce_Spey
|
|
gptkbp:retired
|
gptkb:1980s
1970s
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_RB.168
|
|
gptkbp:turbine_type
|
2
single stage turbine
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gptkbp:type
|
gptkb:turbofan_engine
turbojet
|
|
gptkbp:used_in
|
gptkb:Hawker_Siddeley_Buccaneer
|
|
gptkbp:weight
|
400 kg
1,200 lb
|