Accession Number : ADD002496

Title :   Burning Rate Modifying Binder for Propellant and Method.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON D C

Personal Author(s) : Braun,John D ; Nielsen,Arnold ; Pickett,M Frank ; Henry,Ronald ; Norris,William P

Report Date : 13 Jan 1976

Pagination or Media Count : 4

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.

Descriptors :   *Solid rocket propellant binders, *Burning rate, *Ferrocenes, *Patents, Catalysts, Chemical bonds, Polybutadiene, Curing agents, Hydrogen compounds, Oxides

Subject Categories : Organic Chemistry
      Solid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE