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Detail of some of the "cat eyes" in the middle of the thrust chamber wall.

The J-2 thrust chamber is constructed of 360 full-length "up" tubes running from reverse-flow manifold to the the injector, plus an additional 180 "down" tubes running from the fuel manifold to the reverse-flow manifold. This "pass-and-a-half" construction increases the number of tubes comprising the thrust chamber as the diameter of the nozzle increases, allowing for a high expansion ratio.

The gaps between the sets of "up" tubes both make room for the introduction of the "down" tubes and serve as slots through which the turbine exhaust gas (from the exhaust manifold, just forward of the fuel manifold) enters the combustion chamber. Dumping the turbine exhaust into the thrust chamber in this fashion enhanced the engine's specific impulse.

 
Turbine exhaust manifold outlet slots and down tubes emanating from J-2 Engine fuel manifold at Stennis Space Center
Time picture taken Tue Jun 14 11:21:10 2005
Location picture taken Rocket Park
Visitor Center
Stennis Space Center, MS
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