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Differential charging of high-voltage spacecraft - The equilibrium potential of insulated surfacesA theory is presented for the steady-state potential of insulated surfaces near exposed high voltages. The term 'insulated surfaces' is used to mean either dielectric surfaces or electrically isolated metallic surfaces. The potential is bounded below by the zero of the material's I-V curve assuming total suppression of secondary electrons, and above by assuming total extraction of secondaries. Within these bounds, the material's surface potential is determined consistently with the solution to Poisson's equation external to the vehicle. The theory is compared with rocket experiments and with SCATHA satellite data. Also, an explanation is suggested for the observed 'snapover' of solar cell coverslips from near plasma ground potential to near the potential of positively biased interconnects with increasing bias voltage.
Document ID
19820052012
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Katz, I.
(Systems Science and Software La Jolla, CA, United States)
Mandell, M. J.
(Systems, Science, and Software, La Jolla CA, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1982
Publication Information
Publication: Journal of Geophysical Research
Volume: 87
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
82A35547
Funding Number(s)
CONTRACT_GRANT: NAS3-22536
Distribution Limits
Public
Copyright
Other

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