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gptkbp:instance_of
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gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Hawker_Siddeley_Harrier
gptkb:Folland_Gnat
gptkb:Hawker_Hunter
gptkb:BAC_Strikemaster
gptkb:de_Havilland_Sea_Vixen
|
|
gptkbp:combustor_type
|
axial flow
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
hydraulic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
gptkb:Bristol_Siddeley
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:emissions_standard
|
low emissions
|
|
gptkbp:engine
|
gptkb:military_aircraft
Brayton cycle
|
|
gptkbp:engine_configuration
|
gptkb:Bristol_Siddeley
inline engine
pylon-mounted
single spool
|
|
gptkbp:engine_type
|
afterburning turbojet
|
|
gptkbp:first_flight
|
gptkb:1958
|
|
gptkbp:fuel_capacity
|
1,200 lb
12 ft 6 in
3 ft 4 in
|
|
gptkbp:fuel_economy
|
0.8 lb/hp/hr
0.6 lb/lbf/hr
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bristol Siddeley Orpheus 703 AS
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:introduced
|
gptkb:1958
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Bristol_Siddeley
|
|
gptkbp:max_speed
|
Mach 0.9
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operational_history
|
gptkb:Royal_Air_Force
gptkb:Royal_Navy
|
|
gptkbp:operational_range
|
1,200 miles
|
|
gptkbp:operational_use
|
gptkb:military_aircraft
|
|
gptkbp:power_output
|
3,700 k W
|
|
gptkbp:propulsion
|
4.17
5,000 lbf
|
|
gptkbp:replaced_by
|
gptkb:Rolls-Royce_Spey
|
|
gptkbp:retired
|
gptkb:1980s
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_RB.168
|
|
gptkbp:turbine_type
|
single stage turbine
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:used_in
|
gptkb:Hawker_Siddeley_Buccaneer
|
|
gptkbp:weight
|
1,200 lb
|