Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:combustor_type |
annular
|
| gptkbp:compressor_type |
axial
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:engine |
Brayton cycle
|
| gptkbp:engine_configuration |
turbojet
|
| gptkbp:first_flight |
gptkb:1958
|
| gptkbp:fuel_economy |
0.85 lb/lbf/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric J97
|
| gptkbp:length |
14 ft 6 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:operational_range |
0 to 100% RPM
|
| gptkbp:propulsion |
15,000 lbf
|
| gptkbp:related_aircraft |
gptkb:F-4_Phantom_family
|
| gptkbp:turbine_type |
single spool
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
|
| gptkbp:weight |
3,500 lb
|
| gptkbp:bfsParent |
gptkb:General_Electric_F101
|
| gptkbp:bfsLayer |
5
|