General Electric J79-GE-7 turbojet
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:compressor_type |
axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
3 ft 2 in (0.97 m)
|
| gptkbp:firstRun |
1950s
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:length |
17 ft 7 in (5.36 m)
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notableFeature |
variable stator vanes
|
| gptkbp:notableUser |
gptkb:United_States_Air_Force
gptkb:United_States_Navy |
| gptkbp:numberOfStages |
17
|
| gptkbp:part_of |
gptkb:General_Electric_J79_family
|
| gptkbp:thrust |
yes
|
| gptkbp:thrust_(afterburner) |
17,000 lbf
|
| gptkbp:thrust_(dry) |
10,000 lbf
|
| gptkbp:usedInAircraft |
gptkb:Convair_B-58_Hustler
gptkb:McDonnell_Douglas_F-4_Phantom_II |
| gptkbp:weight |
3,850 lb (1,746 kg)
|
| gptkbp:bfsParent |
gptkb:F-104C
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric J79-GE-7 turbojet
|