METHOD FOR PRODUCING MIXED FIRM ROCKET FUEL Russian patent published in 2017 - IPC C06B21/00 

Abstract RU 2621800 C1

FIELD: chemistry.

SUBSTANCE: manufacturing charges blends with solid fuel missile is carried by the free injection of the fuel mixture from the mixer through the drain system assembled with snap-channeling housing. In the process of forming an additional fuel mixture is filled container docked to the drain system located in the conical part of the adapter by snap-channeling valve, and configured as a cylinder with a piston. After the draining of the fuel mixture from the mixer fuel mixture is forced into the body through the piston of the additional capacity.

EFFECT: reduced loss of the fuel mixture at the expense of guaranteed fuel mixture filling the housing volume located above the drainage holes in the channel forming a snap.

1 dwg

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RU 2 621 800 C1

Authors

Kazakov Aleksandr Alekseevich

Tolmachev Gennadij Alekseevich

Novikov Sergej Anatolevich

Dates

2017-06-07Published

2016-06-28Filed