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Numerical simulation of spacecraft charging phenomenaA numerical simulation program is being constructed having the following features: (1) infinite circular cylindrical geometry with angle-dependence, (2) inclusion of incident particles, photoelectrons, secondary electrons, backscattered electrons, any gun emissions, and any internal current pathways including surface conductive layers, (3) quasistatic time-dependent iteration, in which sheath potential changes during particle transit times are ignored, (4) use of approximate, locally-dependent space charge density expressions in solving Poisson's equation for sheath potentials, with use of numerical orbit-following to determine surface currents, and (5) incident particle velocity distributions isotropic or beam-like, or some superposition of these. Rationales for each of these features are discussed.
Document ID
19780002206
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Laframboise, J. G.
(Young (Arthur) and Co. Bethesda, MD, United States)
Prokopenko, S. M. L.
(Young (Arthur) and Co. Bethesda, MD, United States)
Date Acquired
August 9, 2013
Publication Date
February 24, 1977
Publication Information
Publication: NASA. Lewis Res. Center Proc. of the Spacecraft Charging Technol. Conf.
Subject Category
Ground Support Systems And Facilities (Space)
Accession Number
78N10149
Funding Number(s)
CONTRACT_GRANT: AF-AFOSR-2962-76
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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