Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
6
|
| gptkbp:bfsParent |
gptkb:J79_turbojet
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:engine |
single spool
|
| gptkbp:engine_type |
axial
|
| gptkbp:first_flight |
gptkb:1958
|
| gptkbp:fuel_type |
JP-4
can-type |
| https://www.w3.org/2000/01/rdf-schema#label |
J79-GE-8 K
|
| gptkbp:length |
15 ft 9 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:number_of_stages |
8
|
| gptkbp:operational_range |
0 to 100% RPM
|
| gptkbp:propulsion |
17,000 lbf
|
| gptkbp:successor |
gptkb:F404
|
| gptkbp:type |
turbojet
|
| gptkbp:used_in |
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
|
| gptkbp:variant |
gptkb:J79-GE-15
|
| gptkbp:weight |
2,800 lb
|