Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
3 ft 2 in
|
| gptkbp:engineType |
axial-flow turbojet
|
| gptkbp:firstFlight |
1950s
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric J79-GE-10B
|
| gptkbp:length |
17 ft 7 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notableFeature |
variable stator vanes
|
| gptkbp:numberOfStages |
17
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
yes
17,900 lbf with afterburner |
| gptkbp:usedIn |
gptkb:Convair_B-58_Hustler
gptkb:Lockheed_F-104_Starfighter gptkb:McDonnell_Douglas_F-4_Phantom_II |
| gptkbp:weight |
3,850 lb
|
| gptkbp:bfsParent |
gptkb:F-4S_Phantom_II
|
| gptkbp:bfsLayer |
7
|