Silicone containing solid 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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Details

149 194, 149 199, 149 20, C06B 4510

Patent

active

042104742

ABSTRACT:
Addition of a small amount, for example 1% by weight, of a liquid silicone oil to a metal containing solid rocket propellant provides a significant reduction in heat transfer to the inert nozzle walls eliminating metal oxide slag collection and blockage of the nozzle and increases burning rate by about 5 to 10% improving ballistic performance.

REFERENCES:
patent: 3197349 (1965-07-01), Kuhn et al.
patent: 3260631 (1966-07-01), Witz et al.
patent: 3266959 (1966-08-01), Ackley
patent: 3350245 (1967-10-01), Dickinson
patent: 3715246 (1973-02-01), Sayles
patent: 3781179 (1973-12-01), Huskins et al.
patent: 4158583 (1979-06-01), Frosch

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