Burning Rate Modifying Binder for Propellant and Method.
DEPARTMENT OF THE NAVY WASHINGTON D C
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The patent pertains to solid rocket propellants which use hydroxy terminated polybutadiene as the binder and a reactive burn-rate catalyst selected from 4, 4-diferrocenyl-1-pentanol and 3,3-diferrocenylbutyl isocyanate are disclosed. The burn-rate catalysts are chemically bound to the binder to prevent migration.
- Organic Chemistry
- Solid Rocket Propellants