Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:compressionRatio |
centrifugal-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:General_Electric_I-40
|
| gptkbp:diameter |
33 in
|
| gptkbp:firstFlight |
1944
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:length |
119 in
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:notableFor |
first mass-produced American turbojet engine
|
| gptkbp:numberOfStages |
1
|
| gptkbp:relatedTo |
gptkb:General_Electric_J31
gptkb:General_Electric_J35 |
| gptkbp:status |
retired
|
| gptkbp:thrust |
4,000 lbf
5,400 lbf |
| 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 gptkb:Northrop_F-89_Scorpion |
| gptkbp:weight |
1,820 lb
|
| gptkbp:bfsParent |
gptkb:IHI_J59_engine
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison J33 engine
|