Flow-Restricting Filter, Solid Propellant Gas Generator and Propulsion System Comprising the Same

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United States of America Patent

APP PUB NO 20100024388A1
SERIAL NO

12262774

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Abstract

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The present invention discloses a flow-restricting filter capable of restricting intentionally the flow of the combustion gas from a solid propellant gas generator to an external member (for example, the nozzle) to rise up combustion pressure resulting in increasing a burning rate of the solid propellant and in reducing a burning area of the solid propellant and the overall size of the gas generator. The flow-restricting filter according to the present invention comprises a hollow member having a plurality of through holes formed thereon; and a flow-blocking plate provided at one end of the hollow member to form a space having one closed end and another opened end in the hollow member.

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Patent Owner(s)

Patent OwnerAddress
KOREA AEROSPACE RESEARCH INSTITUTE169-84 GWAHAK-RO YUSEONG-GU DAEJEON 34133

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
HONG, Moon Geun Daejeon-shi, KR 1 0
LEE, Soo Yong Seoul, KR 24 175

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