Structurally-strong solid propellants

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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149 199, 560355, C06B 4510

Patent

active

050470973

ABSTRACT:
A diisocyanate crosslinking agent having a minimum chain length of methylene groups from 25 to 45 which has a coiling-uncoiling ability in a cured solid propellant composition (under stress and relaxing of stress) as a result of the chain length and configuration imparts superior structural strength to the solid propellant composition. A preferred species is 1,37-heptatriacontane diisocyanate, OCN--(CH.sub.2).sub.37 --NCO, which is employed as an effective crosslinking agent in hydroxyl-terminated polybutadiene propellants.

REFERENCES:
patent: 3245849 (1966-04-01), Klager et al.
patent: 3932240 (1976-01-01), Braun et al.
patent: 3932253 (1976-01-01), Mastrolia et al.
patent: 4019933 (1977-04-01), Cucksee et al.
patent: 4133706 (1979-01-01), Shoults
patent: 4142927 (1979-03-01), Walker et al.
patent: 4263071 (1981-04-01), Bain et al.
Hawley, "The Condensed Chemical Dictionary", 9th Ed., p. 302, Van Nostrand einhold Co. (1977), New York.

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