High burning rate tactical solid rocket propellant, and related method

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United States of America Patent

PATENT NO 8986473
SERIAL NO

12283144

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Abstract

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The invention is a composition for a high burning-rate solid rocket propellant, where the composition includes a binder compounded with a soluble energetic additive; a metallic fuel; and an oxidative fuel. The resulting composition has a tactical Class 1.3 hazard rating, and a linear regression rate that is substantially equivalent to a tactical Class 1.1 hazard rating obtainable using solid rocket propellants. The composition may include a heat-conducting element, a plasticizer, a curing component, a combustion catalyst, and curing catalyst.

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Patent Owner(s)

Patent OwnerAddress
UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY THEBALLSTON TOWER ONE 800 NORTH QUINCY STREET CHIEF OF NAVAL RESEARCH OFFICE OF COUNSEL (ATTN CODE OOCCIP) ARLINGTON VA 22217

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Gill, Robert C White Plains, US 13 63
Kelley, John M Owings Mills, US 5 37

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