DocumentCode :
2698303
Title :
The role of space plasma simulation chambers in spacecraft design and testing
Author :
Ferguson, Dale C.
Author_Institution :
Space Environ. Effects Branch, NASA Lewis Res. Center, Cleveland, OH, USA
Volume :
4
fYear :
1996
fDate :
11-16 Aug 1996
Firstpage :
2188
Abstract :
Space plasma simulation chambers have been used, since the earliest days of the space program, to investigate the effects of the space plasma environment on spacecraft systems. A space plasma simulation chamber is a vacuum chamber capable of producing and retaining a high vacuum (10-6 to 10-5 torr) during operation of a plasma source capable of producing a plasma of up to 10 6 electrons and ions per cubic centimeter. Usually, the chamber must be large enough that plasma effects on the spacecraft systems or subsystems to be tested will not be influenced directly by the plasma source or the chamber walls. This means that the chamber must be several times the size of the plasma sheath surrounding the sample even when it is biased to high voltages relative to the surrounding plasma
Keywords :
aerospace test facilities; aerospace testing; astrophysical plasma; design engineering; plasma simulation; 1E-6 to 1E-5 torr; space plasma simulation chambers; spacecraft design; spacecraft testing; vacuum chamber; Electronic equipment testing; Electrons; Plasma measurements; Plasma sheaths; Plasma simulation; Plasma sources; Space shuttles; Space vehicles; System testing; Voltage;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Energy Conversion Engineering Conference, 1996. IECEC 96., Proceedings of the 31st Intersociety
Conference_Location :
Washington, DC
ISSN :
1089-3547
Print_ISBN :
0-7803-3547-3
Type :
conf
DOI :
10.1109/IECEC.1996.561156
Filename :
561156
Link To Document :
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