Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:General_Electric_J79
|
| gptkbp:diameter |
30 in
|
| gptkbp:engine |
turbojet
|
| gptkbp:engine_type |
axial compressor
single-stage turbine |
| gptkbp:first_flight |
gptkb:1958
|
| gptkbp:fuel_capacity |
0.85 lb/lbf/hr
|
| gptkbp:fuel_type |
annular combustor
JP-4 |
| https://www.w3.org/2000/01/rdf-schema#label |
J79-GE-24
|
| gptkbp:length |
14 ft 9 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:operational_range |
0 to 100% RPM
|
| gptkbp:propulsion |
17,000 lbf
|
| gptkbp:successor |
J85
|
| gptkbp:supports |
30 lb/s
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
gptkb:star |
| gptkbp:weight |
1,800 lb
|