Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:check_in_time |
yes
|
| gptkbp:compressor_type |
axial
|
| gptkbp:design |
J93
|
| gptkbp:development |
gptkb:General_Electric
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:engine |
J93 family
|
| gptkbp:first_flight |
gptkb:1958
|
| gptkbp:fuel_type |
gptkb:jet_engine
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric J93-GE-7
|
| gptkbp:length |
15 ft 6 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:operational_use |
1960s
|
| gptkbp:propulsion |
17,000 lbf
|
| gptkbp:successor |
gptkb:General_Electric_F404
|
| gptkbp:turbine_type |
axial
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
|
| gptkbp:weight |
3,000 lb
|
| gptkbp:bfsParent |
gptkb:General_Electric_F101
|
| gptkbp:bfsLayer |
5
|