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General Electric J35

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Engine developed by General Electric as an advanced J33. The J35 was the Air Force's first axial-flow compressor turbojet. Production of the engine was turned over to Allison division of General Motors.

Technical Specifications
Rated Output 6,000 lbs thrust
Compressor 11 stage axial
Turbine 1 stage axial
Dry Weight 2,850 lbs
After Burner 7,200 lbs thrust depending on series
Commonly Used On X-5, XB-43, XB-45, XB-46, XB-47, XB-48, XB-49, F-84B/C/D/E/G, F-89


Location: Restoration