DUAL-MODE SOLID PROPELLANT ROCKET ENGINE Russian patent published in 2022 - IPC F02K9/18 F02K9/26 F02K9/32 

Abstract RU 2783054 C1

FIELD: rocketry.

SUBSTANCE: invention relates to the field of rocketry, namely to solid propellant rocket engines. A dual-mode solid propellant rocket engine comprises a body, a front bottom with an igniter, a rear bottom with a gas duct and a nozzle block, and a solid fuel charge with an internal cylindrical channel having slots on the side of the front bottom and fastened to the body with a protective and fastening layer, while the length of the slots is 0.4-0.7 of the total length of the solid fuel charge, and the ratio of the burning area of ​​the slotted part of the channel is 5-8 to the burning area of ​​the cylindrical part of the channel.

EFFECT: invention provides dual-mode operation of the engine - starting and marching modes of operation, and increasing the reliability of its operation.

1 cl, 2 dwg

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RU 2 783 054 C1

Authors

Vityazev Aleksej Vitalevich

Kabanov Dmitrij Evgenevich

Loginov Andrej Nikolaevich

Naumchenko Ilya Konstantinovich

Sorokin Vladimir Alekseevich

Dates

2022-11-08Published

2022-06-02Filed