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Detailed views of the fuel return manifold and turbine exhaust manifold flow vanes.

Fuel flows down two adjacent tubes, cooling the engine wall (known as "regenerative cooling"). It reaches the fuel return manifold (the silver ring at the exit plane of the thrust chamber), where it returned through two "up" tubes, reaching the fuel manifold and then being injected into the combustion chamber.

The turbine exhaust gasses exit through these flow vanes on the aft end of the turbine exhaust manifold, enter the double-walled nozzle extension, and finally enter the main exhaust flow through gaps in the shingles comprising the nozzle extension inner wall and thus provide film cooling to the nozzle extension.

Picture 2 of 3.

 
F-1 Engine (Davidson Center) at U.S. Space and Rocket Center
Time picture taken Sun Oct 23 12:55:30 2011
Location picture taken Saturn V Hall
Davidson Center for Space Exploration
U.S. Space & Rocket Center
Huntsville, AL
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