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Orbital debris sweeper and methodAn orbital debris sweeper is provided for removing particles from orbit which otherwise may impact and damage an orbiting spacecraft. The debris sweeper includes a central sweeper core which carries a debris monitoring unit, and a plurality of large area impact panels rotatable about a central sweeper rotational axis. In response to information from the debris monitoring unit, a computer determines whether individual monitored particles preferably impact one of the rotating panels or pass between the rotating panels. A control unit extends or retracts one or more booms which interconnect the sweeper core and the panels to change the moment of inertia of the sweeper and thereby the rotational velocity of the rotating panels. According to the method of the present invention, the change in panel rotational velocity increases the frequency of particles which desirably impact one of the panels and are thereby removed from orbit, while large particles which may damage the impact panels pass between the trailing edge of one panel and the leading edge of the rotationally succeeding panel.
Document ID
19910011909
Acquisition Source
Johnson Space Center
Document Type
Other - Patent
External Source(s)
MSC-21534-1
Authors
Andrew J Petro
(Johnson Space Center Houston, United States)
Date Acquired
August 14, 2013
Publication Date
February 12, 1991
Publication Information
Publisher: United States Patent and Trademark Office
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
Patent Number: NASA-CASE-MSC-21534-1
Patent Number: US-PATENT-4,991,788
Patent Application Number: US-PATENT-APPL-SN-480985
Accession Number
91N21222
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,991,788
Patent Application
US-PATENT-APPL-SN-480985
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