Solid rocket propellant

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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149 196, 149 191, 149 76, C06B 4510

Patent

active

06066214&

ABSTRACT:
A solid propellant composition includes an oxidizer, a fuel and a binder, the oxidizer containing a significant amount of bismuth oxide (Bi.sub.2 O.sub.3)

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patent: 5654520 (1997-08-01), Boberg et al.
patent: 5783769 (1998-07-01), Goleniewski et al.

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