Statements (66)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:allies |
awarded multiple military contracts.
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:combustor_type |
annular
|
| gptkbp:compressor_type |
axial
|
| gptkbp:control_system |
manual control.
|
| gptkbp:cooling_system |
air-cooled.
|
| gptkbp:design |
designed for supersonic flight.
engineered by a team at General Electric. |
| gptkbp:development |
developed for the United States Air Force.
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:emissions_standard |
higher emissions compared to modern engines.
|
| gptkbp:engine |
extensive documentation available.
remains a significant part of aviation history. Brayton cycle. General Electric J79. assembled in specialized facilities. part of the J-series engines. upgraded in some military applications. |
| gptkbp:engine_configuration |
turbojet.
detailed in military specifications. focused on maximizing thrust. |
| gptkbp:engine_cooling_technology |
utilized advanced cooling technology.
|
| gptkbp:engine_performance_reviews |
received positive performance reviews.
|
| gptkbp:engine_power |
considered reliable for its time.
evaluated based on thrust and efficiency. |
| gptkbp:engine_type |
no significant variants produced.
|
| gptkbp:first_flight |
gptkb:1956
|
| gptkbp:fuel_economy |
moderate.
high at full throttle. |
| gptkbp:fuel_type |
JP-4
|
| gptkbp:has_units |
approximately 1,000 units.
|
| gptkbp:historical_significance |
important in the evolution of military aviation.
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric J93-GE-5
|
| gptkbp:improves |
incorporated design improvements over time.
|
| gptkbp:influence |
influenced the design of subsequent turbojet engines.
|
| gptkbp:is_tested_for |
extensively tested before deployment.
subjected to rigorous testing protocols. tested at various military testing facilities. |
| gptkbp:legacy |
influenced future jet engine designs.
|
| gptkbp:length |
14 ft 6 in
|
| gptkbp:maintenance |
requires regular maintenance.
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:material |
constructed from high-strength alloys.
|
| gptkbp:noise_level |
high.
|
| gptkbp:notable_features |
high thrust-to-weight ratio.
|
| gptkbp:number_of_rooms |
can withstand high temperatures.
|
| gptkbp:operational_history |
used in various military operations.
|
| gptkbp:operational_range |
limited by fuel capacity.
|
| gptkbp:operational_use |
used primarily by the U. S. military.
|
| gptkbp:performance |
high performance in military applications.
|
| gptkbp:predecessor |
gptkb:General_Electric_J47
|
| gptkbp:production_years |
produced from 1956 to 1960.
|
| gptkbp:propulsion |
17,000 lbf
not equipped. |
| gptkbp:related_aircraft |
compatible with multiple aircraft.
|
| gptkbp:research_and_development |
part of extensive R& D programs.
|
| gptkbp:retired_aircraft |
F-4 Phantom II retired in the 1990s.
|
| gptkbp:retirement |
retired from active service.
|
| gptkbp:successor |
gptkb:General_Electric_J79
|
| 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
|