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Three-dimensional calculation of shuttle charging in polar orbitThe charged particles environment in polar orbit can be of sufficient intensity to cause spacecraft charging. In order to gain a quantitative understanding of such effects, the Air Force is developing POLAR, a computer code which simulates in three dimensions the electrical interaction of large space vehicles with the polar ionospheric plasma. It models the physical processes of wake generation, ambient ion collection, precipitating auroral electron fluxes, and surface interactions, including secondary electron generation and backscattering, which lead to vehicle charging. These processes may be followed dynamically on a subsecond timescale so that the rapid passage through intense auroral arcs can be simulated. POLAR models the ambient plasma as isotropic Maxwellian electrons and ions (0+, H+), and allows for simultaneous precipitation of power-law, energetic Maxwellian, and accelerated Gaussian distributions of electrons. Magnetic field effects will be modeled in POLAR but are currently ignored.
Document ID
19850014175
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cooke, D. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Katz, I.
(NASA Lewis Research Center Cleveland, OH, United States)
Mandell, M. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Lilley, J. R., Jr.
(NASA Lewis Research Center Cleveland, OH, United States)
Rubin, A. J.
(AFGL)
Date Acquired
August 12, 2013
Publication Date
March 1, 1985
Publication Information
Publication: NASA. Lewis Research Center Spacecraft Environ. Interactions Technol., 1983
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
85N22486
Funding Number(s)
CONTRACT_GRANT: F19628-82-C-0081
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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