Title: Rocket propellant with acrylate binder and difluoroamino plasticizer

Abstract: High energy, low radar attenuation propellant comprising (1) 25-55 weight rcent of a binder which itself comprises from 2-25 weight percent of a copolymer of acrylic acid and a lower alkyl acrylate and 75-98 weight percent of an energetic difluoroamino group containing plasticizer, (2) 0-15 weight percent aluminum or boron (3) 45-75 weight percent of an oxidizer and (4) 1/2-5 weight percent curing agent.

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Inventors: Childs, Jr., Lewis B. (Vienna, VA, US)
Martin, James D. (Alexandria, VA, US)

Application Number: 263892
Filing Date: 1972-06-16
Publication_date: 1976-01-20
Assignee: The United States of America as represented by the Secretary of the Navy (Washington, DC)
Primary Class(es): 149/19.3 149/19.91, 149/20
Other Classes:
US Patent Ref:

3663323	May, 1972	Engel et al.	149/19.
3666576	May, 1972	Engel	149/19.
3813305	May, 1974	Baldwin et al.	149/19.

Other Refs:
Primary Examiner: Miller, Edward A.
Assistant Examiner:
Attorney: