|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:de_Havilland_Sea_Vixen
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:combustor_type
|
axial flow
|
|
gptkbp:compressor_type
|
8
|
|
gptkbp:control_system
|
hydromechanical
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:engine
|
gptkb:military_aircraft
gptkb:Bristol_Siddeley_Orpheus_family
performance upgrades
limited production
Brayton cycle
afterburner
1950s technology
developed in the UK
|
|
gptkbp:engine_configuration
|
gptkb:Bristol_Siddeley
inline
single spool
detailed specifications available.
|
|
gptkbp:engine_power
|
high
good
|
|
gptkbp:engine_type
|
afterburning turbojet
Orpheus 703
Orpheus 703, Orpheus 703 A
|
|
gptkbp:first_flight
|
gptkb:1958
|
|
gptkbp:fuel_capacity
|
0.9 m
3.1 m
400 kg
|
|
gptkbp:fuel_economy
|
0.8 kg/k N/h
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bristol Siddeley Orpheus 703 AB
|
|
gptkbp:ignition_system
|
gptkb:spark_plug
|
|
gptkbp:introduced
|
gptkb:1958
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:length
|
3.1 m
|
|
gptkbp:maintenance
|
moderate
|
|
gptkbp:manufacturer
|
gptkb:Bristol_Siddeley
|
|
gptkbp:max_speed
|
Mach 0.9
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:notable_users
|
gptkb:Royal_Navy
|
|
gptkbp:propulsion
|
0.55
22 k N
|
|
gptkbp:related_aircraft
|
gptkb:BAC_TSR-2
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_RB.168
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:used_in
|
gptkb:Hawker_Siddeley_Buccaneer
|
|
gptkbp:weight
|
400 kg
|