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New NASA SEE LEO Spacecraft Charging Design Guidelines: How to Survive in LEO Rather Than GEOIt has been almost two solar cycles since the 1984 GEO Guidelines of Purvis, Garrett, Whittlesey, and Stevens were published. In that time, interest in high voltage LEO systems has increased. Correct and conventional wisdom has been that LEO conditions are sufficiently different from GEO that the GEO Guidelines (and other GEO and POLAR documents produced since then) should not be used for LEO spacecraft. Because of significant recent GEO spacecraft failures that have been shown in ground testing to be likely to also occur on LEO spacecraft, the SEE program commissioned the production of the new LEO Spacecraft Charging Design Guidelines. Now available in CD-ROM form, the LEO Guidelines highlight mitigation techniques to prevent spacecraft arcing on LEO solar arrays and other systems. We compare and contrast the mitigation techniques for LEO and GEO in this paper. We also discuss the extensive bibliography included in the LEO Guidelines, so results can be found in their primary sources.
Document ID
20040026971
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Ferguson, Dale C.
(NASA Glenn Research Center Cleveland, OH, United States)
Hillard, G. Barry
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
December 1, 2003
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA/TM-2003-212737
E-14262
Report Number: NASA/TM-2003-212737
Report Number: E-14262
Meeting Information
Meeting: Eigth Spacecraft Charging Technology Conference
Location: Huntsville, AL
Country: United States
Start Date: October 20, 2003
End Date: October 24, 2003
Sponsors: NASA Marshall Space Flight Center, European Space Agency, Air Force Research Lab.
Funding Number(s)
WBS: WBS 22-755-04-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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