Bristol Siddeley Orpheus 703 AL
GPTKB entity
Statements (64)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:aircraft_operated |
gptkb:Folland_Gnat
gptkb:Hawker_Sea_Hawk gptkb:Hawker_Hunter gptkb:BAC_Lightning gptkb:de_Havilland_Sea_Vixen Bristol 188 |
| gptkbp:combustor_type |
axial flow
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:control_system |
hydraulic control
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:engine |
Brayton cycle
air start |
| gptkbp:engine_configuration |
pylon-mounted
single spool |
| gptkbp:engine_type |
afterburning turbojet
Orpheus 703 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 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 AL
|
| gptkbp:ignition_system |
spark ignition
|
| gptkbp:length |
14 ft 6 in
|
| gptkbp:manufacturer |
gptkb:Bristol_Siddeley
|
| gptkbp:operational_history |
used by Indian Air Force
used by Royal Air Force used by Royal Navy used by South African Air Force used by Pakistan Air Force |
| gptkbp:propulsion |
4.67
7000 lbf |
| gptkbp:successor |
gptkb:Rolls-Royce_Spey
|
| gptkbp:turbine_type |
single stage turbine
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:Hawker_Siddeley_Buccaneer
|
| gptkbp:weight |
1500 lb
|