DocumentCode
790306
Title
Plasma ESD Qualification Test Procedure of Alcatel Alenia Space Solar Array
Author
Berthou, C. ; Boulanger, B. ; Lévy, Leon
Author_Institution
Alcatel Alenia Space, Cannes
Volume
34
Issue
5
fYear
2006
Firstpage
2004
Lastpage
2010
Abstract
The detrimental effects of spacecraft charging are well known, particularly when the charging leads to arcing on solar array and, consequently, to permanent power loss. Motivated by these concerns, Alcatel Alenia Space has undertaken several test campaigns to qualify solar array design and to investigate margins. This paper describes the state-of-the-art Alcatel Alenia Space solar array electrostatic discharge laboratory test setup and procedure. The primary discharges are created using a plasma source and negative polarization of the sample rear side. The required power to feed the arc can be delivered by a solar array simulator with low-capacitance power sources. The test sample is fully representative of a flight model
Keywords
aerospace simulation; arcs (electric); electrostatic discharge; solar cell arrays; spacecraft charging; Alcatel Alenia Space solar array; flight model; low-capacitance power sources; plasma ESD qualification test procedure; power loss; primary discharges; solar array design; solar array electrostatic discharge laboratory test setup; solar array simulator; spacecraft charging; Circuit testing; Electrons; Electrostatic discharge; Fault location; Laboratories; Plasma sources; Qualifications; Silicon; Space charge; Space vehicles; Arcing; electrostatic discharge (ESD); solar array; solar array simulator (SAS);
fLanguage
English
Journal_Title
Plasma Science, IEEE Transactions on
Publisher
ieee
ISSN
0093-3813
Type
jour
DOI
10.1109/TPS.2006.883371
Filename
1710076
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