DocumentCode :
990554
Title :
Modeling of FEEP Plume Effects on MICROSCOPE Spacecraft
Author :
Roussel, Jean-François ; Tondu, Thomas ; Matéo-Vélez, Jean-Charles ; Chesta, Enrico ; Escrivan, Stéphane D. ; Perraud, Laurent
Author_Institution :
Space Environ. Dept., French Nat. Aerosp. Res. Establ., Toulouse
Volume :
36
Issue :
5
fYear :
2008
Firstpage :
2378
Lastpage :
2386
Abstract :
Several aspects of plume effects of field-effect electric propulsion (FEEP) were studied. We first estimated the contamination by cesium deposit due to charge exchange of fast ions and slow neutrals and to direct neutral impingement. Levels are rather low, with local maximums of a few tens or hundreds of angstroms per year, and not much more than 1-10 Aring farther from thruster nozzles. Neutralization of the ions emitted by FEEPs was also addressed, both concerning FEEP ion space-charge compensation and spacecraft net current, i.e., the floating potential issue. With the presence of a cathode-grounded neutralizer, the spacecraft was shown to float somewhat negatively with little dependence on the ambient environment.
Keywords :
aerospace propulsion; artificial satellites; caesium; charge exchange; ion engines; positive ions; Cs; Cs+ ion density; FEEP plume effects modeling; MICROSCOPE spacecraft; cathode-grounded neutralizer; fast ions; field-effect electric propulsion; space-charge compensation; spacecraft net current; Chemicals; Coatings; Gravity; Microscopy; Orbits; Plasma chemistry; Polymers; Propulsion; Space vehicles; Surface contamination; Cesium; field-effect electric propulsion (FEEP); floating potential; space vehicle propulsion; surface contamination;
fLanguage :
English
Journal_Title :
Plasma Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0093-3813
Type :
jour
DOI :
10.1109/TPS.2008.2002541
Filename :
4675222
Link To Document :
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