Rocket propellant with acrylate binder and difluoroamino plastic

Details Rocket propellant with acrylate binder and difluoroamino plastic Rocket propellant with acrylate binder and difluoroamino plastic

1972-06-16

1976-01-20

Miller, Edward A.

Explosive and thermic compositions or charges

Structure or arrangement of component or product

Solid particles dispersed in solid solution or matrix

149 1991, 149 20, C06D 506

Patent

active

039335429

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.

REFERENCES:
patent: 3663323 (1972-05-01), Engel et al.
patent: 3666576 (1972-05-01), Engel
patent: 3813305 (1974-05-01), Baldwin et al.

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