Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:compressionRatio |
axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:General_Electric_I-40
|
| gptkbp:diameter |
33 in
|
| gptkbp:firstFlight |
1943
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:length |
119 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notableFor |
first mass-produced American turbojet engine
|
| gptkbp:numberOfStages |
8
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Allison_J35
|
| gptkbp:thrust |
5400 lbf
4000 lbf |
| gptkbp:usedDuring |
gptkb:Korean_War
gptkb:World_War_II |
| gptkbp:usedInAircraft |
gptkb:Convair_XF-92
gptkb:Ryan_X-13_Vertijet gptkb:McDonnell_XF-88_Voodoo gptkb:Lockheed_F-94_Starfire gptkb:Lockheed_P-80_Shooting_Star |
| gptkbp:weight |
1,820 lb
|
| gptkbp:bfsParent |
gptkb:IHI_J33_engine
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
General Electric J33
|