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High-temperature catalyst for catalytic combustion and decompositionA robust, high temperature mixed metal oxide catalyst for propellant composition, including high concentration hydrogen peroxide, and catalytic combustion, including methane air mixtures. The uses include target, space, and on-orbit propulsion systems and low-emission terrestrial power and gas generation. The catalyst system requires no special preheat apparatus or special sequencing to meet start-up requirements, enabling a fast overall response time. Start-up transients of less than 1 second have been demonstrated with catalyst bed and propellant temperatures as low as 50 degrees Fahrenheit. The catalyst system has consistently demonstrated high decomposition effeciency, extremely low decomposition roughness, and long operating life on multiple test particles.
Document ID
20080005104
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Patent
Authors
Mays, Jeffrey A.
Lohner, Kevin A.
Sevener, Kathleen M.
Jensen, Jeff J.
Date Acquired
August 24, 2013
Publication Date
May 3, 2005
Subject Category
Chemistry And Materials (General)
Report/Patent Number
Patent Number: US-PATENT-6,887,821
Patent Application Number: US-PATENT-APPL-SN-405019
Funding Number(s)
CONTRACT_GRANT: NCC8-193
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-6,887,821
Patent Application
US-PATENT-APPL-SN-405019
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