Cooling Jacket with Porous Matrix
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United States of America Patent
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Issued Date -
Oct 24, 2013
app pub date -
Apr 4, 2013
filing date -
Dec 8, 2008
priority date (Note) -
Abandoned
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Abstract
The fluids and heat transfer theory for regenerative cooling of a rocket combustion chamber with a porous media coolant jacket is presented. This model is useful for calculating temperature distributions in a coolant fluid and combustion chamber or heat source as well as the associated fluid pressure drop through the coolant jacket. This model for fluids and heat transfer theory can be used to design a regeneratively cooled rocket engine.
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