Method of making rocket engine combustion chamber utilizing "slide in" port liner
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United States of America Patent
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Dec 30, 1997
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N/A
app pub date -
Jun 23, 1994
filing date -
Jun 23, 1994
priority date (Note) -
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Abstract
A method of fabricating a rocket engine combustion chamber comprising assembling a liner having cooling channels, a plurality of throat support sections, and a structural jacket having inlet and outlet manifolds. Then heating the assembly in a pressurized furnace to bond the assembled parts to each other.
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