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Поисковые слова: propulsion

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- .. akishin@hep.sinp.msu.ru The arcing causes degradation of solar array at malfunction of instruments on satellites. The discharge is caused by differential potential between satellite body and insulator surfaces like coverglass of solar arrays, whitch are charged by ambient plasma.

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1. S.Hosoda , T.Okumura , K.Toyoda , M,Cho . Development of 400V. Solar Array Technology for Low Earth Orbit Plasma Environment. // IEEE Trans on Plasma Science, 2006, v. 34, 5, p.1986-1996. 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. 2011-2030. 3. D.C.Ferguson, G.B.Hillard. Low Earth Orbit Spacecraft Charging Design Guidelines. NASA/TP -2003-2112287, p.1-44. 4. http://www.sat-nd.com/launchfailures/8. 5. I.A.Rodiek, H.W.Brandhorst., I.M.O'Neill. Stretched Lens Array (SLA), A Reliable Solar Array for Any Orbit. Prospector XII ­Space Solar Array Cost Workshop, Park City, Utah. 6. ..., .., .., ..., .., .. ,.. ., ... // ,1990,1,.75-76. 7. .. , .. ., .. ., .. . . // , 1991, 4, 23-26. 8. .. , .. , .. . // ,1991,4,.68-71. 9. .. , .., .., .. // ,1994,3,.28-30. 10. ... . // , 1995, N 2, . 43-48 11. .., .., .. . . // , 1996, N6, . 20-23 12. .. . . . .II, . . .. . .. . . , 2007, . 561-594. 13. K.Toyoda, T.Matsumoto , M.Cho . Power Reduction of Solar Arrays by Arcing Under Simulated Geosynchronous Orbit Environment. // J. of Spacecraft and Rockets Vol. 41, No. 5, 2004. p. 14. J.Katz ,V.A.Davis V,,D.B.Snyder , E.A.Robertson. ESD triggered Solar Array failure mechanism. 6 th Spacecraft Technology Conf. AFRL-VS-TR-20001578, 1 Sept. 2000, p.39. 15. .. . . : -,2004,.704. 16. M.J.O'Neil , A.J.McDanal , M.F.Piszczor,, D.I.Edwards , M.I.Eskenazi , Brandhorst H,W, Recent Technology Advances for the Stretched Lens Arrays ( SLA )., A Space Solar offering state of the Art Performance at Low cost and Ultra-light mass. 31st IEEE Photovoltaic Specialists Conf.-Orlando, Florida-Jan., 2005. 17. M.J.O'Neil, 1,000 w/kg Solar Concentrator Arrays for Far-Term Space Missions. Space Technology Applications International Forum ( STAIF) ­Albuquerque-Febr.2004, p,1-8, 18. 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, Italy, Sept. 2007. 19. 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.