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Active spacecraft potential control for Cluster - implementation and first results

Torkar, K., Riedler, W., Escoubet, C.P., Fehringer, M., Schmidt, R., Grard, R.J., Arends, H., Rudenauer, F., Steiger, W., Narheim, B.T., Svenes, K., Torbert, R., Andre, M., Fazakerley, A., Goldstein, R., Olsen, R.C., Pedersen, A., Whipple, E. and Zhao, H. (author)
Uppsala universitet,Institutionen för astronomi och rymdfysik
 (creator_code:org_t)
2001
2001
English.
In: Annales Geophysicae. ; 9:10-12, s. 1289-1302
  • Journal article (peer-reviewed)
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  • Electrostatic charging of a spacecraft modifies the distribution of electrons and ions before the particles enter the sensors mounted on the spacecraft body. The floating potential of magnetospheric satellites in sunlight very often reaches several tens o

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