High-temperature catalyst for catalytic combustion and decomposition
AssigneeThe Boeing Company
InventorsJeffrey A. Mays, Kevin A. Lohner, Kathleen M. Sevener, Jeff J. Jensen
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AssigneeThe Boeing Company
InventorsJeffrey A. Mays, Kevin A. Lohner, Kathleen M. Sevener, Jeff J. Jensen
Estimating the term…
A 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.
A robust, high-activity catalyst for use in high-temperature decomposition of propellants, including 70-99% hydrogen peroxide, the catalyst comprising:
A robust, high-activity catalyst for use in high-temperature decomposition of propellants, including 70-99% hydrogen peroxide, the catalyst comprising:
A method for forming a robust, high-temperature catalyst material for use in decomposing propellants or catalytic combustion in the power and propulsion industry, the method comprising:
A robust, high-activity activated catalyst for use in high-temperature decomposition of propellants, including 70-99% hydrogen peroxide, the activated catalyst comprising:
A robust, high-activity activated catalyst for use in high-temperature decomposition of propellants, including 70-99% hydrogen peroxide, the activated catalyst comprising:
A method for forming a robust, high-temperature activated catalyst material for use in decomposing propellants or catalytic combustion in the power and propulsion industry, the method comprising:
Dependencies are inferred from the claim text.