Äîêóìåíò âçÿò èç êýøà ïîèñêîâîé ìàøèíû. Àäðåñ îðèãèíàëüíîãî äîêóìåíòà : http://nuclphys.sinp.msu.ru/school/s09/09_56.pdf Äàòà èçìåíåíèÿ: Wed Oct 21 14:26:15 2009 Äàòà èíäåêñèðîâàíèÿ: Tue Oct 2 00:29:48 2012 Êîäèðîâêà:

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- .. akishin@hep.sinp.msu.ru The problems caused by charging on satellites have been compared to other environmental effects. Some of the main results of this study are summarized in Table I, which indicates that satellite charging is responsible for more than half of the documented environment related anomalies. The study results also showed, that electrostatic discharges caused about 50% of the lost or terminated missions associated with environmental effects. Thus, the issue of satellite charging is very serious from the perspective of the threat it poses for satellites in the inner magnetosphere.

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1. J F..Fennell , H,C.Koons ., J.I.Roeder ., J.B.Blake . Spacecraft Charging:Observation and Relationship to SatelliteAnomalie http://articles.adsabs.harvard.edu//full/2001ESASP.476..279F/0000279.000.html 2. M.Cho, J.Kim, S.Hosoda, Y.Nozaki, T.Miura, T.Iwata. Electrostatic Discharge Ground Test of a Polar Orbit Satellite Solar Panel. IEEE Trans.on Plasma Science, 2006,v.34, 5, p.20112030 3. 3.. T.Kawasaki ,S. Hosoda , J Kim , K. Toyoda , M. Cho. Charge Neutralization via Arcing on a Large Solar Array in the GEO Plasma Environment // IEEE Trans, on Plasma Science, 2006.v.34, 5, .1979-1985. 4. Jr,H.W. Brandhorst, S.R.Best, I.A. Rodiek, M.I.O'Neil , M.I. Eskenazi, D.C.Ferguson Advances in Radiation-Tolerant Solar Arrays for SEP Missions. The 30th International Electric Propulsion Conf., Florence. 5. ..,... .., ., ., , 1985. 6, 73. 6. .. . // , 2002, 4, .44-50. 7. .. . .//, 2000, 3, .24-31 8. S.T. Lai, E.Murad. Hazards Hypervelosity Impacts on Spacecraft, JSR, 2002, v.39, 1, p.106-114. 9. D.C.Ferguson.,.B.G.Hillard.. Low Earth Orbit Spacecraft Charging Design Guidelines. NASA/TR -2003-2112287, p.1-44. 10. A.I.Eriksson., J.Wahlund. Charging of the Freja Satellite in the Auroral Zone. IEEE Trans.on Plasma Scence , 2006,v.34, 6, p.2038-2044.


11. .. ., . . , 2008 , 4, .21-28. 12. .. . - // . .,2005, 3, .5-11 13. .. . // , 2003, 5, .28-31 14. .. . . // , 1995, N 2, . 43-48 15. .. , .. , .. , .. , .. , .. , .. , .. . // ,1990, 1,.75-76. 16. .. . // , 2004, 2, .35-38. 17. S.T. Lai. A Critical Overview on Spacecraft Charging Mitigation Methods .IEEE Trans. Plasma Science, 2003, v.31, 6, .1118-1124.