Accession Number:

ADD002496

Title:

Burning Rate Modifying Binder for Propellant and Method.

Descriptive Note:

Patent,

Corporate Author:

DEPARTMENT OF THE NAVY WASHINGTON D C

Report Date:

1976-01-13

Pagination or Media Count:

4.0

Abstract:

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.

Subject Categories:

  • Organic Chemistry
  • Solid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE