Burning rate modifying binder for propellant and method

Details Burning rate modifying binder for propellant and method Burning rate modifying binder for propellant and method

1973-06-04

1976-01-13

Lechert, Jr., Stephen J.

Explosive and thermic compositions or charges

Structure or arrangement of component or product

Solid particles dispersed in solid solution or matrix

149 199, 149 42, 149 76, 260439CY, C06B 4510

Patent

active

039322408

ABSTRACT:
Solid rocket propellants which utilize hydroxy terminated polybutadiene as he 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.

REFERENCES:
patent: 3813304 (1974-05-01), Reed
patent: 3843426 (1974-10-01), Huskins et al.

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