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Rocket Combustion Chamber CoatingA coating with the ability to protect (1) the inside wall (i.e., lining) of a rocket engine combustion chamber and (2) parts of other apparatuses that utilize or are exposed to combustive or high temperature environments. The novelty of this invention lies in the manner a protective coating is embedded into the lining.
Document ID
20020034152
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Patent
External Source(s)
MFS-31438-1
Authors
Richard R Holmes
(Marshall Space Flight Center Redstone Arsenal, United States)
Timothy N McKechnie
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
August 20, 2013
Publication Date
November 13, 2001
Publication Information
Publisher: United States Patent and Trademark Office
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-6,314,720
Patent Application
US-Patent-Appl-SN-490290
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