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Wall structure for rocket engine, has two layers to carry significant portion of structural load, where one layer exhibits higher thermal conductivity and lower thermal expansion than another layer
Wall structure for rocket engine, has two layers to carry significant portion of structural load, where one layer exhibits higher thermal conductivity and lower thermal expansion than another layer
The structure has a layer (6) located closer to a source of thermal load than another layer (5). The two layers are arranged such that heat is allowed to conduct from layer (6) to the layer (5). The two layers carry a significant portion of a structural load. The layer (6) exhibits a higher thermal conductivity and a lower thermal expansion than the layer (5).
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