Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:compressor_type |
axial
|
| gptkbp:diameter |
30 in
|
| gptkbp:engine |
Brayton cycle
|
| gptkbp:first_flight |
gptkb:1958
|
| gptkbp:first_introduced |
gptkb:1956
|
| gptkbp:fuel_economy |
0.85 lb/hp/hr
|
| gptkbp:fuel_type |
JP-4
|
| https://www.w3.org/2000/01/rdf-schema#label |
J79-GE-15
|
| gptkbp:length |
14 ft 9 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:max_speed |
Mach 2.2
|
| gptkbp:operational_use |
gptkb:Vietnam_War
|
| gptkbp:propulsion |
15,000 lbf
3.95 |
| gptkbp:related_aircraft |
gptkb:F-4_Phantom_family
|
| gptkbp:successor |
gptkb:J79-GE-17
|
| gptkbp:turbine_type |
single spool
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
|
| gptkbp:variant |
J79-GE-15 A
|
| gptkbp:weight |
3,800 lb
|
| gptkbp:bfsParent |
gptkb:General_Electric_J79
|
| gptkbp:bfsLayer |
5
|