gptkbp:instance_of
|
gptkb:jet_engine
|
gptkbp:application
|
gptkb:military_aircraft
|
gptkbp:average_temperature
|
1500 K
|
gptkbp:combustor_type
|
annular
|
gptkbp:compressor_type
|
axial
|
gptkbp:control_system
|
hydraulic
|
gptkbp:cooling_system
|
air-cooled
|
gptkbp:development
|
1950s to 1960s
|
gptkbp:diameter
|
1.1 m
|
gptkbp:emissions_standard
|
ICAO Chapter 3
|
gptkbp:engine
|
Brayton cycle
|
gptkbp:engine_configuration
|
turbojet
inline
Orpheus 703
|
gptkbp:engine_type
|
Orpheus 703 A
Orpheus 703 B
Orpheus 703 C
Orpheus 703 D
Orpheus 703 E
Orpheus 703 F
Orpheus 703 G
Orpheus 703 H
Orpheus 703 I
Orpheus 703 J
Orpheus 703 K
Orpheus 703 L
Orpheus 703 M
Orpheus 703 N
Orpheus 703 O
Orpheus 703 P
Orpheus 703 Q
Orpheus 703 R
Orpheus 703 S
Orpheus 703 T
Orpheus 703 U
Orpheus 703 V
Orpheus 703 W
Orpheus 703 X
Orpheus 703 Y
Orpheus 703 Z
|
gptkbp:first_flight
|
gptkb:1958
|
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 AW
|
gptkbp:ignition_system
|
gptkb:spark_plug
|
gptkbp:involved_technology
|
afterburner
|
gptkbp:length
|
3.4 m
|
gptkbp:maintenance
|
500 hours
|
gptkbp:manufacturer
|
gptkb:Bristol_Siddeley
|
gptkbp:max_speed
|
Mach 0.9
|
gptkbp:noise_level
|
85 d B
|
gptkbp:number_of_stages
|
8
|
gptkbp:operational_use
|
1960s
|
gptkbp:propulsion
|
7000 lbf
8.75
|
gptkbp:related_aircraft
|
gptkb:Folland_Gnat
|
gptkbp:service_ceiling
|
12,000 m
|
gptkbp:successor
|
gptkb:Rolls-Royce_RB.168
|
gptkbp:turbine_type
|
single-stage
|
gptkbp:type
|
gptkb:turbofan_engine
|
gptkbp:used_in
|
gptkb:Hawker_Siddeley_Buccaneer
|
gptkbp:weight
|
800 kg
|