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Regeneratively Cooled Porous Media JacketThe fluid and heat transfer theory for regenerative cooling of a rocket combustion chamber with a porous media coolant jacket is presented. This model is used to design a regeneratively cooled rocket or other high temperature engine cooling jacket. Cooling jackets comprising impermeable inner and outer walls, and porous media channels are disclosed. Also disclosed are porous media coolant jackets with additional structures designed to transfer heat directly from the inner wall to the outer wall, and structures designed to direct movement of the coolant fluid from the inner wall to the outer wall. Methods of making such jackets are also disclosed.
Document ID
20140001874
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Mungas, Greg
Fisher, David J.
London, Adam Pollok
Fryer, Jack Merrill
Date Acquired
March 14, 2014
Publication Date
April 9, 2013
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
Patent Number: US-Patent-8,413,419
Patent Application Number: US-Patent-Appl-SN-12/633,770
Funding Number(s)
CONTRACT_GRANT: NNX09CB12C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-8,413,419
Patent Application
US-Patent-Appl-SN-12/633,770
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