METHOD OF PRODUCING MIXED ROCKET SOLID PROPELLANT PRODUCT Russian patent published in 2009 - IPC C06B21/00 

Abstract RU 2361850 C1

FIELD: fuel systems.

SUBSTANCE: method of producing the mixed rocket propellant product attached to the casing comprises injection moulding the product, solidifying it under pressure, cooling to below equilibrium temperature and pressing out moulding attachments from the product. Note that the said pressing-out is carried out at the special pressing-out unit till complete removal of aforesaid attachments by stepwise pressure reduction in hydraulic cylinders of aforesaid unit, the pressure being kept at every step for 2 to 15 minutes. At the first pressing-out step, hydraulic cylinder pressure is 3 to 10% higher than that of the hydraulic cylinder no-load operation. At every following step, pressure is increased to exceed by 5 to 10% the pressure of previous step.

EFFECT: reduced loads, acting on structural elements in pressing out.

1 tbl, 1 ex

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RU 2 361 850 C1

Authors

Kutsenko Gennadij Vasil'Evich

Salakhov Radus Fassakhovich

Salakhov Rafis Fassakhovich

Fedoseev Jurij Alekseevich

Fedchenko Nikolaj Nikolaevich

Vinokurov Jurij Anatol'Evich

Bozh'Ja-Volja Nikolaj Sergeevich

Dates

2009-07-20Published

2007-10-02Filed