Rocket engine combustion chamber with enhanced heat transfer to cooling jacket
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United States of America Patent
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Oct 28, 2003
Grant Date -
Jul 18, 2002
app pub date -
Nov 2, 2001
filing date -
Nov 2, 2000
priority date (Note) -
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Abstract
A combustion chamber for a rocket engine expels a hot stream of gas and has a cooling device. The inner wall of the combustion chamber adjoins the cooling device and contains depressions formed in such a way that the stable outer layer of the stream of gas that forms in the proximity of the inner wall of the combustion chamber during operation of the combustion chamber is destabilized in the area of the depressions.
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