GEO Spacecraft Worst-Case Charging Estimation by Numerical Simulation

J.C. Matéo-Vélez 1 C. Pignal 1 N. Balcon 2 D. Payan 2 P. Sarrailh 1 S.L.G. Hess 1
1 Toulouse - ONERA - The French Aerospace Lab
2 CNES - Centre National d'Etudes Spatiales
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.
Keywords : SPACECRAFT CHARGING WORST-CASE ENVIRONMENT RADIATION INDUCED CONDUCTIVITY
Type de document :
Communication dans un congrès
Spacecraft Charging Technology Conference 2014 (13th SCTC), Jun 2014, PASADENA, United States
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Dernière modification le : mercredi 28 mars 2018 - 14:16:10
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J.C. Matéo-Vélez, C. Pignal, N. Balcon, D. Payan, P. Sarrailh, et al.. GEO Spacecraft Worst-Case Charging Estimation by Numerical Simulation. Spacecraft Charging Technology Conference 2014 (13th SCTC), Jun 2014, PASADENA, United States. 〈hal-01070320〉

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