Low velocity injector manifold for hypergolic rocket engine

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 9404441
APP PUB NO 20100037590A1
SERIAL NO

12193679

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Abstract

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A fuel manifold for a thrust chamber assembly includes a main fuel chamber which is generally frustro-conical in shape. The main fuel chamber provides a resonance frequency that is different than an acoustic resonance frequency of a combustion chamber.

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Patent Owner(s)

Patent OwnerAddress
AEROJET ROCKETDYNE OF DE INCP O BOX 13222 SACRAMENTO CA 95813-6000

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Brown, William S Newbury Park, US 7 22
Dodd, Frederick Oak Park, US 2 3
Noble, Rodney Lancaster, US 3 10
Walczuk, Thomas M Oak Park, US 4 20

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