Author: SPINE
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Potential Barrier in the Electrostatic Sheath Around Geotail, Cluster and BepiColombo spacecraft
Thiébault, B., A. Hilgers, E. Sasot, V. Génot, P. Escoubet and H. Laakso, J. Forest, Potential Barrier in the Electrostatic Sheath Around Geotail, Cluster and BepiColombo spacecraft, in Proceedings of 9th Spacecraft Charging Technology Conference, Tsukuba, Japan, JAXA-SP-05-001E, April 2005.
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A corrector for spacecraft calculated electron moments
Geach, J., S.J. Schwartz, V. Génot, O. Moullard, A. Lahiff, and A. N. Fazakerley, A corrector for spacecraft calculated electron moments, Ann. Geophysicae, 23(3), 931, 2005.https://doi.org/10.5194/angeo-23-931-2005
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9th SPINE meeting
Attendees | Attendees data Introduction The development of a new Spacecraft-Plasma Interaction modelling Software (SPIS) was started within SPINE community in December 2002. The motivations and requirements for this software development were recalled during the 4th SPINE Meeting. The first software developments and Working Group activities for software testing and appropriation were reported during the…
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Potential barrier in the electrostatic sheath around a magnetospheric spacecraft
Thiébault, B., Hilgers, A., Sasot, E., Laakso, H., Escoubet, P., Génot, V., and Forest, J. (2004), “Potential barrier in the electrostatic sheath around a magnetospheric spacecraft”, J. Geophys. Res., 109, A12207, doi:10.1029/2004JA010398.
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8th SPINE meeting
Attendees | Attendees data Introduction The development of a new Spacecraft-Plasma Interaction modelling Software (SPIS) was started within SPINE community in December 2002. The motivations and requirements for this software development were recalled during the 4th SPINE Meeting. The first software developments and Working Group activities for software testing and appropriation were reported during the…
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Electrodynamic Tethers in Space
Lorenzini, E. C., and J.R.Sanmartín, Scientific American, Electrodynamic Tethers in Space, 291, no. 2, Aug 2004
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Spacecraft potential effects on electron moments derived from a perfect plasma detector
Génot, V. and Schwartz, S. J.: Spacecraft potential effects on electron moments derived from a perfect plasma detector, Ann. Geophys., 22, 2073–2080, 2004.doi: https://doi.org/10.5194/angeo-22-2073-2004
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A study of the electrical charging of the Rosetta orbiter: 2. Experimental tests in a laboratory plasma
Berthelier, J.‐J., and Roussel, J.‐F. (2004), A study of the electrical charging of the Rosetta orbiter: 2. Experimental tests in a laboratory plasma, J. Geophys. Res., 109, A01105, doi:10.1029/2003JA009834
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A study of the electrical charging of the Rosetta orbiter: 1. Numerical model
Roussel, J.‐F., and Berthelier, J.‐J. (2004), “A study of the electrical charging of the Rosetta orbiter: 1. Numerical model”, J. Geophys. Res., 109, A01104, doi:10.1029/2003JA009836.
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European Approach to material characterisation for plasma characterisation analysis
VanEesbeek, M., A. Hilgers, B. Dirassen, L. Levy, I. Montero, L. Galan, European Approach to material characterisation for plasma characterisation analysis, in Proceedings of the 8th Spacecraft Charging Technology Conference, Huntsville, AL, USA, October 20-24, 2003, NASA/CP-2004-213091.