FIELD: rocketry.
SUBSTANCE: the method for destruction of charges of solid propellant or its fragment located in the body of the rocket engine consists in filling of the charge cavities with refrigerant - waterhelium composition based on polyacrylamide and burning up of the charge. The waterhelium composition based on polyacrylamide is prepared by separate introduction of aqueous solutions of the components of the redox system of solidification-potassium bichromte and sodium thiosulfate in equal volume of aqueous solution of polyacrylamide, and the cavities of the charge are filled by synchronous feeding of the obtained volumes through a mixing head, after that solidification is performed.
EFFECT: provided controlled burning up of charges.
2 dwg, 2 tbl, 1 ex
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Authors
Dates
2005-01-27—Published
2003-06-24—Filed