Explosive and thermic compositions or charges – Processes of making
Patent
1985-12-04
1988-01-12
Lechert, Jr., Stephen J.
Explosive and thermic compositions or charges
Processes of making
75 68C, 149124, D03D 2300
Patent
active
047189550
ABSTRACT:
Solid composite propellants for rocket motors normally consist of an oxidizer and and aluminum powder cured in a polymeric binder system. The oxidizer, ammonium perchlorate, can be readily removed by suitable solvents leaving a residue consisting primarily of aluminum and polymer. The aluminum and polymer are separated by a process that is based upon the differential oxidation of the polymer leaving the aluminum in its original powder form. Aluminum metal forms, on exposure to air, an extremely tough inert aluminum oxide coating. Because of this, aluminum is extremely resistant to further oxidation even at temperatures up to its melting point at 660.degree. C. Most organic compounds, including polymers, are oxidized to carbon dioxide at much lower temperatures (400.degree.-600.degree. C.). Due to this difference in reactivity, it is possible to remove the polymer from the aluminum as carbon dioxide leaving the aluminum residue.
REFERENCES:
patent: 3165397 (1965-01-01), Lobo
patent: 3867296 (1975-02-01), Hunt
patent: 4548651 (1985-10-01), Ramsey
Lechert Jr. Stephen J.
Morton Thiokol Inc.
White Gerald K.
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