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Large space system: Charged particle environment interaction technologyLarge, high voltage space power systems are proposed for future space missions. These systems must operate in the charged-particle environment of space and interactions between this environment and the high voltage surfaces are possible. Ground simulation testing indicated that dielectric surfaces that usually surround biased conductors can influence these interactions. For positive voltages greater than 100 volts, it has been found that the dielectrics contribute to the current collection area. For negative voltages greater than-500 volts, the data indicates that the dielectrics contribute to discharges. A large, high-voltage power system operating in geosynchronous orbit was analyzed. Results of this analysis indicate that very strong electric fields exist in these power systems.
Document ID
19790014017
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stevens, N. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Roche, J. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Grier, N. T.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1979
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
E-012
NASA-TM-79156
Report Number: E-012
Report Number: NASA-TM-79156
Meeting Information
Meeting: Conf. on Advanced Technol. for Future Space Systems
Location: Hampton, VA
Country: United States
Start Date: May 8, 1979
End Date: May 11, 1979
Sponsors: AIAA
Accession Number
79N22188
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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