Protection and Mitigation

The Technical Scheme of Integrated Structure for Shielding and Perception for Spacecraft

  • XU Xin ,
  • DENG Wei-hua ,
  • GONG Zi-zheng ,
  • ZHANG Pin-liang ,
  • LIU Jiang
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  • 1. DFH Satellite Co.,Ltd,China Academy of Space Technology,Beijing 100094,China;
    2. Beijing Institute of Spacecraft Environment Engineering,Beijing 100094,China

Online published: 2023-12-12

Abstract

Except for the space station,China's spacecraft have not been designed for space debris shielding,and thus being faced with the serious threat of hypervelocity impact of space debris.Based on the existing high strength advanced shielding materials in China and aiming at the integrated structure of shielding and perception for spacecraft,we have been exploring the integration of the space debris shielding,insulation,perception and other functions into the spacecraft structure,establishing comprehensive evaluation method for integrated structure of spacecraft.

Cite this article

XU Xin , DENG Wei-hua , GONG Zi-zheng , ZHANG Pin-liang , LIU Jiang . The Technical Scheme of Integrated Structure for Shielding and Perception for Spacecraft[J]. Journal of Space Science and Experiment, 2022 , 22(2) : 11 -17 . DOI: 10.19963/j.cnki.2096-4099.2022.02.002

References

[1] 龚自正,杨继运,张文兵,等.航天器空间碎片超高速撞击防护的若干问题[J].航天器环境工程,2007,24(3):125-130.
[2] 龚自正,李明.美俄卫星太空碰撞事件及对航天器活动的影响[J].航天器环境工程,2009,26(2):101-106.
[3] ESA Space Debris Office.ESA's annual space environ-ment report revision 3.2[R].2019.
[4] Christophe Bonnal,Darren S,Mc Knight.IAA situation report on space debris-2016[R].CNES,ISBN/EANIAA:978-2-917761-56-4.2017.
[5] 龚自正、赵秋艳、李明,等.空间碎片防护研究前沿问题与展望[J].空间碎片研究,2019,19(3):2-13.
[6] J-C Liou.Recent breakup of a DMSP satellite[J].Orbital Debris Quarterly News,2015,19(2).
[7] J-C Liou.Recent NOAA-16 satellite breakup[J].Orbital Debris Quarterly News,2016,20(1&2).
[8] 龚自正,陈川,曹燕,等.低轨大规模星座的机遇与挑战[R].威海:第十届全国空间碎片学术交流会,2019.
[9] Jae-Hwang Lee,Phillip ELoya,JunLou,et al.Dyna-mic mechanical behavior of multilayer graphene via supersonic projectile penetration[J].Science,2014,345(6213):1092-1096.
[10] Marc Davidson,Scott Roberts,Gerhard Castro,et al.Investigating amorphous metal composite architectures as spacecraft shielding[J].Advanced Engineering Materials,DOI:10.1002/adem.201200313.
[11] 宋光明,李明,武强,等.超高速撞击下波阻抗梯度防护结构碎片云特性研究 [J].爆炸与冲击,2021,2:69-80.
[12] 宋光明,李明,龚自正,等.梯度分布对波阻抗梯度材料超高速撞击特性影响实验研究[R].桐乡:第十二届全国爆炸力学学术会议论文集,2018.
[13] 武强,张庆明,龙仁荣,等.含能材料防护屏在球形弹丸超高速撞击下的穿孔特性研究[J].兵工学报,2017,38(11):127-133.
[14] CHRISTIANSEN E L.Meteoroid/debris shielding:TP-2003-210788 [R].2003.
[15] 王青林.基于PVDF的空间碎片在轨感知技术研究 [D].哈尔滨:哈尔滨工业大学,2012.
[16] A J Tuzzolino.Two-dimensional position-sensing PVDF dust detectors for measurements of dust particle trajectory,velocity and mass [J].Nuclear Intruments and Methods in Physics Research,1991,301(3):558-567.
[17] J Kim,JK Ryou ,SJ Kim.Optimal gain distribution for two dimensions modal transducer and its implementation using multi-layered PVDF films [J].Journal of Sound and Vibrantion,2002,251(3):395-408.
[18] 申景诗.基于光纤传感的航天器结构在轨状态监测技术研究 [D].西安:西安电子科技大学,2019.
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