Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:compressionRatio |
axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
3 ft 2 in
|
| gptkbp:firstFlight |
1955
|
| gptkbp:fuelType |
gptkb:gasoline
|
| gptkbp:length |
17 ft 7 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notableFor |
used in supersonic military aircraft
|
| gptkbp:numberOfStages |
17
|
| gptkbp:relatedTo |
gptkb:General_Electric_J79
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
yes
17,900 lbf |
| gptkbp:usedIn |
gptkb:Convair_B-58_Hustler
gptkb:North_American_A-5_Vigilante gptkb:Lockheed_F-104_Starfighter gptkb:McDonnell_Douglas_F-4_Phantom_II gptkb:IHI_F-104J |
| gptkbp:weight |
3,850 lb
|
| gptkbp:bfsParent |
gptkb:F-104S
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric J79-GE-19
|