Solid rocket propellant

Details Solid rocket propellant Solid rocket propellant

2005-06-14

2005-06-14

Felton, Aileen (Department: 3641)

Explosive and thermic compositions or charges

Structure or arrangement of component or product

Solid particles dispersed in solid solution or matrix

C149S124000

Reexamination Certificate

active

06905561

ABSTRACT:
A solid rocket propellant includes a hydroxy-terminated caprolactone ether binder and an oxidizer. The propellant may be disposed of by contacting it with an aqueous solution of 12 N NaOH or 6 N HCl at a temperature of about 140° F. for about 24 hours to decompose the binder. Solids remaining in the solution after the binder decomposes are removed.

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