Sunlight illumination models for spacecraft surface charging
Grey, Stuart and Marchand, Richard and Ziebart, Marek and Omar, Roghaiya (2017) Sunlight illumination models for spacecraft surface charging. IEEE Transactions on Plasma Science. ISSN 1939-9375 (https://doi.org/10.1109/TPS.2017.2703984)
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Abstract
A model is developed to compute solar illumination of satellite components while accounting for multiple reflections, variable surface properties and illumination source size. This model is implemented in OpenCL and integrated with the parti- cle in cell (PIC) satellite-environment simulation code, PTetra, enabling kinetic simulations in which photoelectron emission resulting from direct illumination and multiple reflections are taken into account. Results for the Solar Orbiter spacecraft show a small change to the overall charging and a significant change to the charge distribution around the Solar Wind Analyzer instrument.
ORCID iDs
Grey, Stuart ORCID: https://orcid.org/0000-0001-9274-0601, Marchand, Richard, Ziebart, Marek and Omar, Roghaiya;-
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Item type: Article ID code: 61023 Dates: DateEvent29 May 2017Published29 May 2017Published Online8 May 2017Accepted31 July 2016SubmittedNotes: (c) 2017 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other users, including reprinting/ republishing this material for advertising or promotional purposes, creating new collective works for resale or redistribution to servers or lists, or reuse of any copyrighted components of this work in other works. Subjects: Science > Physics Department: Faculty of Engineering > Mechanical and Aerospace Engineering Depositing user: Pure Administrator Date deposited: 21 Jun 2017 10:21 Last modified: 11 Nov 2024 11:34 URI: https://strathprints.strath.ac.uk/id/eprint/61023