Explosive and thermic compositions or charges – Structure or arrangement of component or product – Solid particles dispersed in solid solution or matrix
Patent
1971-07-06
1982-06-01
Miller, Edward A.
Explosive and thermic compositions or charges
Structure or arrangement of component or product
Solid particles dispersed in solid solution or matrix
149 194, 149 20, C06B 4510
Patent
active
043326323
ABSTRACT:
A solid rocket propellant comprising (1) ammonium perchlorate, (2) alumin (3) poly(1,2-butylene) glycol, (4) the reaction product of propylene oxide and either trimethylolpropane, hexanetriol or mixtures thereof, (5) 2,3-dihydroxypropyl bis(2-cyanoethyl) amine, (6) hexamethylene diisocyanate, (7) copper chromite, (8) a carboxylic acid ester of either a diol and a monocarboxylic acid or a dicarboxylic acid and a monofunctional alcohol, and (9) sulfur and optionally containing (10) a metal acetylacetonate, (11) 2,4-pentanedione and (12) liquid silicon oil.
REFERENCES:
patent: 3245849 (1966-04-01), Klazer et al.
patent: 3291660 (1966-12-01), Oberth et al.
patent: 3350245 (1967-10-01), Dickinson
patent: 3919011 (1975-11-01), Oberth et al.
patent: 4000023 (1976-12-01), Oberth et al.
Conyers John A.
Oberth Adolph E.
Santerre George M.
Branning A. L.
McDonnell T. E.
Miller Edward A.
Sciascia R. S.
The United States of America as represented by the Secretary of
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