DRAG-BASED PROPELLANT-LESS SMALL SATELLITE ATTITUDE ORBIT AND DE-ORBIT CONTROL SYSTEM

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20200189769A1
SERIAL NO

16324396

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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In an example embodiment, an attitude, orbit, and de-orbit control system (AODCS) for a satellite is provided. In an example embodiment, the AODCS system comprises one or more selectively retractable booms. The one or more selectively retractable booms are collectively configured to provide a selectively adjustable drag during de-orbiting of a satellite over a predefined de-orbiting time.

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Patent Owner(s)

Patent OwnerAddress
UNIVERSITY OF FLORIDA RESEARCH FOUNDATION INCORPORATED223 GRINTER HALL GAINESVILLE FL 32611

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bevilacqua, Riccardo Gainesville, US 1 0
Clark, Scott Kennedy Space Center, US 48 1629
Fineberg, Laurence Kennedy Space Center, US 1 0
Guglielmo, David C Gainesville, US 1 0
Johnson, Yusef Kennedy Space Center, US 1 0
Omar, Sanny Gainesville, US 1 0
Poffenberger, Bradley Kennedy Space Center, US 1 0
Treptow, Justin Kennedy Space Center, US 1 0

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