Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:combustionChambers |
8
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
33 in
|
| gptkbp:firstFlight |
1946
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison J35-A-17D
|
| gptkbp:length |
147 in
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:numberOfStages |
11
|
| gptkbp:partOf |
Allison J35 family
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
5,200 lbf
|
| gptkbp:type |
axial-flow turbojet
|
| gptkbp:usedIn |
gptkb:F-84_Thunderjet
gptkb:F-89_Scorpion XB-47 Stratojet |
| gptkbp:weight |
2,400 lb
|
| gptkbp:bfsParent |
gptkb:F-84E
gptkb:F-84E_Thunderjet |
| gptkbp:bfsLayer |
7
|