Active spacecraft potential control for Cluster – implementation and first results
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 of volts, making measurements of the c...
Main Authors: | K. Torkar, W. Riedler, C. P. Escoubet, M. Fehringer, R. Schmidt, R. J. L. Grard, H. Arends, F. Rüdenauer, W. Steiger, B. T. Narheim, K. Svenes, R. Torbert, M. André, A. Fazakerley, R. Goldstein, R. C. Olsen, A. Pedersen, E. Whipple, H. Zhao |
---|---|
Format: | Article |
Language: | English |
Published: |
Copernicus Publications
2001-09-01
|
Series: | Annales Geophysicae |
Online Access: | https://www.ann-geophys.net/19/1289/2001/angeo-19-1289-2001.pdf |
Similar Items
-
Spacecraft potential control for Double Star
by: K. Torkar, et al.
Published: (2005-11-01) -
Spacecraft potential control aboard Equator-S as a test for Cluster-II
by: K. Torkar, et al.
Published: (1999-12-01) -
<i>Introduction</i><br>The Cluster mission
by: C. P. Escoubet, et al.
Published: (2001-09-01) -
An experiment to study and control the Langmuir sheath around INTERBALL-2
by: K. Torkar, et al.
Published: (1998-09-01) -
Cluster PEACE observations of electrons of spacecraft origin
by: S. Szita, et al.
Published: (2001-09-01)