Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:aircraft_operated |
gptkb:military_aircraft
|
| gptkbp:combustor_type |
axial flow
|
| gptkbp:compression_ratio |
6:1
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:design_date |
post-World War II
|
| gptkbp:diameter |
3 ft 6 in
|
| gptkbp:engine |
gptkb:de_Havilland_Ghost_100
|
| gptkbp:engine_configuration |
single spool
|
| gptkbp:engine_type |
turbojet
|
| gptkbp:first_flight |
1953
|
| gptkbp:fuel_type |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
de Havilland Ghost 500
|
| gptkbp:length |
12 ft 6 in
|
| gptkbp:manufacturer |
gptkb:de_Havilland
|
| gptkbp:notable_feature |
high thrust-to-weight ratio
|
| gptkbp:operational_history |
1953-1960s
|
| gptkbp:propulsion |
5000 lbf
|
| gptkbp:successor |
de Havilland Ghost 600
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:de_Havilland_Comet
|
| gptkbp:weight |
1200 lb
|
| gptkbp:bfsParent |
gptkb:de_Havilland_Ghost
|
| gptkbp:bfsLayer |
7
|