SMALL SATELLITE PROPULSION SYSTEM UTILIZING LIQUID PROPELLANT ULLAGE VAPOR

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United States of America Patent

APP PUB NO 20170363044A1
SERIAL NO

15184854

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A novel approach provides a small satellite propulsion system that uses vapor to generate thrust for the small satellite. The vapor naturally sits on top of liquid propellant(s), which are stored within a propellant tank. The vapor may flow from the propellant tank and through a membrane to interact with a reacting surface to generate thrust.

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Patent Owner(s)

Patent OwnerAddress
THE AEROSPACE CORPORATION2310 EAST EL SEGUNDO BLVD MS M1/040 EL SEGUNDO CA 90245

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Rhodes, Brandie L Redondo Beach, US 2 6

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