Solid-rocket propellants
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United States of America Patent
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Dec 26, 2017
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app pub date -
Jan 4, 2017
filing date -
Mar 9, 2015
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Abstract
Solid-fuel rocket propellants comprising an oxidizer, an oxophilic metal-halophilic metal formulation, and a binder are described herein. Further described are processes for preparing such propellants and methods of reducing hydrogen chloride production via the combustion of such propellants. Non-limiting examples of such formulations include aluminum-lithium alloys.
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