Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:developer |
gptkb:J79_engine
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:engine |
turbojet
|
| gptkbp:engine_type |
axial
single spool |
| gptkbp:first_flight |
gptkb:1956
|
| gptkbp:fuel_capacity |
0.85 lb/lbf/hr
|
| gptkbp:fuel_type |
annular
kerosene |
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric J93
|
| gptkbp:length |
15 ft 6 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:operational_history |
used in various military applications
|
| gptkbp:propulsion |
up to 18,000 lbf
|
| gptkbp:retired |
1990s
|
| gptkbp:successor |
gptkb:General_Electric_F404
|
| gptkbp:type |
gptkb: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
|