Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:US_Air_Force
|
| gptkbp:diameter |
35 in
|
| gptkbp:firstFlight |
1946
|
| gptkbp:length |
147 in
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:notableFor |
first axial-flow turbojet engine mass-produced in the US
|
| gptkbp:numberOfStages |
2
11 |
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Allison_J71
|
| gptkbp:thrust |
4,000 lbf
|
| gptkbp:type |
axial-flow turbojet
|
| gptkbp:usedInAircraft |
gptkb:Convair_XF-92
gptkb:Lockheed_T-33 gptkb:Lockheed_F-94_Starfire gptkb:Republic_F-84_Thunderjet gptkb:Douglas_XB-43_Jetmaster gptkb:North_American_XB-45 |
| gptkbp:weight |
2,400 lb
|
| gptkbp:bfsParent |
gptkb:Martin_XB-48
gptkb:P-136_Thunderjet gptkb:P-84_Thunderjet gptkb:Republic_F-84_Thunderjet |
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison J35
|