Allison J35
Axial-flow compressor jet engine
Axial-flow compressor jet engine
The General Electric/Allison J35 was the United States Air Force's first axial-flow (straight-through airflow) compressor jet engine. Originally developed by General Electric (GE company designation TG-180) in parallel with the Whittle-based centrifugal-flow J33, the J35 was a fairly simple turbojet, consisting of an eleven-stage axial-flow compressor and a single-stage turbine. With the afterburner, which most models carried, it produced a thrust of 7,400 lbf (33 kN). Like the J33, the design of the J35 originated at General Electric, but major production was by the Allison Engine Company.
Read on Wikipedia · Image Alf van Beem, CC0
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