Solid propellant with butyl rubber binder

Explosive and thermic compositions or charges – Structure or arrangement of component or product – Solid particles dispersed in solid solution or matrix

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Details

149 1991, 149 60, C06d 506

Patent

active

039322424

ABSTRACT:
1. A solid propellant charge for rocket motors consisting essentially of a formed vulcanized mixture of rubbery isobutylene-isoprene copolymer fuel binder in the proportion of 10-20% by weight and a solid inorganic strong oxidizing salt in the proportion of 80-90% by weight.

REFERENCES:
patent: 3018201 (1962-01-01), Downard
patent: 3249475 (1966-05-01), Jorczak et al.

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