SOLID PROPELLANT ROCKET ENGINE Russian patent published in 2015 - IPC F02K9/08 

Abstract RU 2554685 C2

FIELD: engines and pumps.

SUBSTANCE: invention relates to rocketry and can be used for development of various-purpose rockets, particularly, space rockets for rescue purposes. Proposed engine consists of two solid propellant charges tightly secured to cases of channel-slot shape and connected by adapter with gas ducts and nozzles. Shaped slots of both channels slots are turned relative to each other about charge lengthwise axes through angle equal to half the spacing there between. Inlet of every nozzle is built in gas duct by 0.1-0.2 of diameter of inlet into gas duct.

EFFECT: pressure drop in combustion chamber, decreased passive weight of rocket engine body.

6 dwg

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RU 2 554 685 C2

Authors

Apakidze Jurij Valentinovich

Petrusev Viktor Ivanovich

Pojarkov Il'Ja Petrovich

Protasova Irina Vasil'Evna

Rytik Sergej Vasil'Evich

Snesar' Vladimir Ivanovich

Chopornjak Anton Dmitrievich

Shishkov Al'Bert Alekseevich

Dates

2015-06-27Published

2013-05-29Filed