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GEO Spacecraft Worst-Case Charging Estimation by Numerical Simulation
Abstract : This paper presents a numerical estimation of spacecraft surface charging that combines the effects of both spacecraft material properties and severe environments, often called worst-cases. A series of simulations with the SPIS-GEO tool (Spacecraft Plasma Interaction Software) is analysed in order to determine if a worst-case environment can be extracted from the literature. The simulation especially focuses on the conductivity parameters, especially radiation induced. It is found hardly feasible to define a single and global worst-case, applicable to all situations.
Cited literature [13 references]
https://hal-onera.archives-ouvertes.fr/hal-01070320
Contributor : Véronique Soullier <>
Submitted on : Wednesday, October 1, 2014 - 9:52:05 AM
Last modification on : Thursday, July 25, 2019 - 4:34:16 PM
Document(s) archivé(s) le : Friday, April 14, 2017 - 11:43:46 AM
Contributor : Véronique Soullier <>
Submitted on : Wednesday, October 1, 2014 - 9:52:05 AM
Last modification on : Thursday, July 25, 2019 - 4:34:16 PM
Document(s) archivé(s) le : Friday, April 14, 2017 - 11:43:46 AM
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DESP14017.1408624199.pdf
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