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微小空间碎片与原子氧协同效应研究 被引量:3

Research of Combined Effect of Small Space Debris and Atomic Oxygen
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摘要 利用等离子体驱动微小碎片加速器和潘宁源的原子氧模拟装置在中国首次开展了微小碎片撞击与原子氧协同作用对Kapton膜和镀铝Kapton膜的侵蚀效应研究.实验结果表明,碎片撞击能明显加剧原子氧对Kapton和镀铝Kapton膜的侵蚀效应,对航天器的寿命及可靠性构成威胁,制约中国长寿命高可靠性航天器的发展. Using plasma drag particulate accelerator and atomic oxygen device based on PIG ion source, the first experiment was carried out about the combined effect of small debris and atomic oxygen on both the standard Kapton and Kapton with aluminum film. The result indicates that hypervelocity impact by particulate can accelerate the erosion effect of atomic oxygen on both Kapton and Kapton with aluminum film. The combined effect of hypervelocity impact and atomic oxygen is more important on Kapton with aluminum film than Kapton without film. This is because the impact by hypervelocity particles can destroy the aluminum film which prevents the atomic oxygen from eroding Kapton. So when consider the atomic oxygen effect on Kapton with aluminum film, the combined effect of hypervelocity impact by space debris and atomic oxygen should not be neglected. As a result, this effect is a threat to the life-span and credibility of spacecraft, which will restrict the development of high credibility and long life spacecraft.
出处 《空间科学学报》 CAS CSCD 北大核心 2011年第4期503-508,共6页 Chinese Journal of Space Science
基金 国家高技术研究发展计划项目资助(2006AA04Z412)
关键词 原子氧 微小碎片 协同效应 Atomic oxygen, Small space debris, Combined effect
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  • 1刘瑞源,吴健,张北辰.电离层天气预报研究进展[J].电波科学学报,2004,19(z1):35-40. 被引量:9
  • 2李涛,姜利祥,刘阳,刘国青.航天器迎风面不同位置原子氧掏蚀效应的数值模拟研究[J].航天器环境工程,2008,25(4):315-318. 被引量:6
  • 3李涛,姜利祥,刘向鹏.表面缺陷对原子氧掏蚀效应影响的数值模拟研究[J].航天器环境工程,2006,23(2):94-97. 被引量:3
  • 4初文毅,杨士勤,何世禹,李丹明.原子氧对Kapton/Al薄膜性能影响研究[J].航空材料学报,2006,26(1):29-31. 被引量:9
  • 5Finckenor M M, Edwards L D, Vaughu J A, et al. Test andAnalysis Capabilities of the Space Environment EffectsTeam at Marshall Space Flight Center [R]. NASA/TP-2002-212076.
  • 6Toru S, Ken'ichiro I,Toshio W, et al. MU radar observa-tions of space debris [C]//Proceedings of the 4th Interna-tional Space Conference of Pacific-basin Societies. Kyoto:Pacific-basin Societies, 1991. 273-282.
  • 7Kessler D J. Orbital debris environment for spacecraft inlow earth Orbit [J]. J. Spacecr. Rocket: 1991, 28(3):347-351.
  • 8Toru S, Takuji N. Orbit determination of meteors usingthe MU radar [J]. IEICE Trans. Commun., 2000, E83-B(9):1990-1995.
  • 9Ono K, Tajima T, Mizutani A, et al Development ofthe first Japanese space debris observation radar [C]//TheThird European Conference on Space Debris. Noordwijk,Netherlands: ESA Publication Division, 2001. 265-272.
  • 10Foster J L, Stansbery E G, Matney M J, et al. Haystackand Hax Radar Measurements of the Orbital Debris En-vironment, 1999-2002 [R]. NASA/JSC-49875, 2003.

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