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gptkbp:instance_of
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gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:combustion_chamber
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
electronic control
hydraulic
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:engine
|
gptkb:fighter_aircraft
gptkb:historical_significance
supercharged
air-start
1950s technology
Bristol Siddeley Orpheus series
|
|
gptkbp:engine_bearing
|
journal bearing
|
|
gptkbp:engine_configuration
|
gptkb:single
turbojet
rear-mounted
|
|
gptkbp:engine_fan
|
no fan
|
|
gptkbp:engine_inlet
|
subsonic inlet
|
|
gptkbp:engine_legacy_systems
|
used in various aircraft.
|
|
gptkbp:engine_power
|
high performance
|
|
gptkbp:engine_replacement
|
gptkb:Rolls-Royce_engines
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
naval aircraft
Orpheus 703 A
|
|
gptkbp:exhaust_system
|
straight exhaust
|
|
gptkbp:first_flight
|
gptkb:1958
|
|
gptkbp:fuel_economy
|
moderate
|
|
gptkbp:fuel_type
|
gptkb:gasoline
kerosene
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bristol Siddeley Orpheus 703 AY
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:impact
|
gptkb:civil_aviation
|
|
gptkbp:length
|
3.6 m
|
|
gptkbp:maintenance
|
scheduled maintenance
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Bristol_Siddeley
|
|
gptkbp:noise_level
|
high
|
|
gptkbp:operational_use
|
gptkb:military_aircraft
|
|
gptkbp:propulsion
|
7000 lbf
8.75
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_RB.168
|
|
gptkbp:turbine_type
|
single-stage
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:used_in
|
gptkb:Hawker_Siddeley_Buccaneer
|
|
gptkbp:variant
|
Orpheus 703
|
|
gptkbp:weight
|
800 kg
|