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Effects of secondary electron emission on chargingLaboratory charging studies using two electron sources with different energies show that the charging behaviors of typical spacecraft thermal control dielectric surface are extremely sensitive to the shape of their secondary emission curves. The results also suggest that the electron spectrum in a natural charging environment can be separated into three distinct regions (noninteracting, discharging, and charging) depending on the kinetic energy of the incident electron relative to the charged surface, and on the secondary emission characteristics of the material. To a first order approximation, the relative number of electrons in these different regions determines the potential of the charged surface. Detailed measurements of the secondary electron emission characteristics of Kapton, the effects of bulk conductivity and secondary emission on surface charging of these materials is reported.
Document ID
19820006352
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Leung, M. S.
(Aerospace Corp. El Segundo, CA, United States)
Tueling, M. B.
(Aerospace Corp. El Segundo, CA, United States)
Schnauss, E. R.
(Aerospace Corp. El Segundo, CA, United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1981
Publication Information
Publication: NASA. Lewis Research Center Spacecraft Charging Technol., 1980
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
82N14225
Funding Number(s)
CONTRACT_GRANT: F04701-80-C-0081
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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