Statements (49)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Spey_202
|
| gptkbp:aircraft_operated |
Phantom family
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:certification |
certified by UKCAA
|
| gptkbp:controls |
hydromechanical
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:engine |
advanced aerodynamics
high reliability twin-engine Brayton cycle high thrust-to-weight ratio 3000 hours wing-mounted air start upgraded versions available influenced future jet engine designs designed for supersonic flight developed from earlier Spey models extensive research and testing conducted military turbojet remains in use in some military applications |
| gptkbp:engine_type |
axial
single spool compatible with various airframes Spey 555 Spey 250 Spey 800 |
| gptkbp:first_flight |
gptkb:1964
|
| gptkbp:fuel_capacity |
0.8 lb/hp/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
annular |
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Spey 400
|
| gptkbp:impact |
significant impact on military aviation
|
| gptkbp:length |
12 ft 6 in
|
| gptkbp:maintenance |
moderate maintenance
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:noise_level |
low noise
|
| gptkbp:notable_users |
gptkb:Mc_Donnell_Douglas_Phantom_II
gptkb:Hawker_Siddeley_Buccaneer BACTSR-2 |
| gptkbp:operational_area |
British military
|
| gptkbp:origin |
gptkb:United_Kingdom
|
| gptkbp:propulsion |
4000 lbf
|
| gptkbp:successor |
gptkb:Rolls-Royce_RB.163
|
| gptkbp:weight |
1200 lb
|
| gptkbp:year_created |
gptkb:1964
|