Volume 30 Issue 3
Jul 2016
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LIU Xian-Ying, GAI Fang-Fang, LI Zhi-Qiang, WANG Zhi-Hua. Characteristic Parameters of Debris Cloud Produced by HypervelocityImpact of Conical Projectiles on Spacecraft Shield[J]. Chinese Journal of High Pressure Physics, 2016, 30(3): 249-257. doi: 10.11858/gywlxb.2016.03.011
Citation: LIU Xian-Ying, GAI Fang-Fang, LI Zhi-Qiang, WANG Zhi-Hua. Characteristic Parameters of Debris Cloud Produced by HypervelocityImpact of Conical Projectiles on Spacecraft Shield[J]. Chinese Journal of High Pressure Physics, 2016, 30(3): 249-257. doi: 10.11858/gywlxb.2016.03.011

Characteristic Parameters of Debris Cloud Produced by HypervelocityImpact of Conical Projectiles on Spacecraft Shield

doi: 10.11858/gywlxb.2016.03.011
  • Received Date: 03 Apr 2015
  • Rev Recd Date: 08 Jun 2015
  • Space debris of different shapes, when impacting spacecraft protection structures, may produce debris clouds which in turn cause secondary damage on the spacecraft.Therefore, it is of great necessity to investigate the characteristics of debris clouds formed from hypervelocity impact by space debris of diverse shapes.We selected 2 aerospace materials, Al 2017-T4 and Al 2A12, respectively as the impacting projectile and the spacecraft shield material, and performed numerical simulations utilizing the smoothened particle hydrodynamics (SPH) technique with the nonlinear dynamic analysis software AUTODYN-2D.We investigated numerically the characteristics of debris clouds, which were generated by the hypervelocity impact of conical projectiles with the same mass and striking velocity but different length-radius ratios normally on the single protective plate in the conical bottom and tip directions.The results show that the axial velocity of the tip particle, the radial diameter and the axial length of debris clouds, and the diameter of the perforation hole are affected by the length-radius ratio and the impact direction of conical projectiles, and their changing regularities are established in the pres

     

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  • [1]
    闵桂荣, 肖名鑫.防止微流星击穿航天器舱壁的可靠性设计[J].中国空间科学技术, 1986(6):45-48. http://www.cnki.com.cn/Article/CJFDTOTAL-ZGKJ198606005.htm

    MIN G R, XIAO M X.Reliability design spacecraft module wall against meteoroid perforation[J].Chinese Space Science and Technology, 1986(6):45-48. http://www.cnki.com.cn/Article/CJFDTOTAL-ZGKJ198606005.htm
    [2]
    张伟, 庞宝君, 邹经湘, 等.航天器微流星体及空间碎片防护方案[J].哈尔滨工业大学学报, 1999, 32(2):18-22. doi: 10.3321/j.issn:0367-6234.1999.02.006

    ZHANG W, PANG B J, ZOU J X, et al.Meteoroid and space shielding concepts for spacecraft[J].Journal of Harbin Institute of Technology, 1999, 32(2):18-22. doi: 10.3321/j.issn:0367-6234.1999.02.006
    [3]
    董洪建, 童靖宇, 黄本诚.真空环境下空间碎片超高速撞击试验研究[J].真空科学与技术学报, 2004, 24(2):109-112. doi: 10.3969/j.issn.1672-7126.2004.02.007

    DONG H J, TONG J Y, HUANG B C.Impact simulation of hypervelocity space debris in vacuum environment[J].Vacuum Science and Technology, 2004, 24(2):109-112. doi: 10.3969/j.issn.1672-7126.2004.02.007
    [4]
    曲广吉, 韩增尧.空间碎片超高速撞击动力学建模与数值仿真技术[J].中国空间科学技术, 2002, 22(5):26-29. doi: 10.3321/j.issn:1000-758X.2002.05.005

    QU G J, HAN Z Y.Dynamical modeling and numerical simulation of hypervelocity space debris impact[J].Chinese Space Science and Technology, 2002, 22(5):26-29. doi: 10.3321/j.issn:1000-758X.2002.05.005
    [5]
    何茂坚. 球形弹丸超高速正撞击薄铝板碎片云特性研究[D]. 哈尔滨: 哈尔滨工业大学, 2007.

    HE M J.Characteristics of debris cloud produced by normal hypervelocity impact of spherical projectile with thin aluminum plate[D].Harbin:Harbin Institute of Technology, 2007.
    [6]
    CORVONATO E, DESTEFANIS R, FARAUD M.Integral model for the description of the debris cloud structure and impact[J].Int J Impact Eng, 2001, 26(1):115-128. http://www.sciencedirect.com/science/article/pii/S0734743X01000744
    [7]
    盖芳芳, 刘先应, 刘恂, 等.圆柱形弹丸高速撞击薄板的碎片云特性数值模拟[J].黑龙江科技学院学报, 2013(6):600-604. http://d.old.wanfangdata.com.cn/Periodical/hljkyxyxb201306022

    GAI F F, LIU X Y, LIU X, et al.Numerical simulation on characteristics of debris clouds produced by cylindrical projectile hypervelocity impact on thin plates[J].Journal of Heilongjiang Institute of Science & Technology, 2013(6):600-604. http://d.old.wanfangdata.com.cn/Periodical/hljkyxyxb201306022
    [8]
    张锁春.光滑质点流体动力学(SPH)方法(综述)[J].计算物理, 1996, 13(4):385-397. http://cdmd.cnki.com.cn/Article/CDMD-10217-2007119005.htm

    ZHANG S C.Smoothed particle hydrodynamics (SPH) method (overview)[J].Chinese Journal of Computational Physics, 1996, 13(4):385-397. http://cdmd.cnki.com.cn/Article/CDMD-10217-2007119005.htm
    [9]
    AUTODYN user's manual revision 6.0[M].Concord, California, USA:Century Dynamics Incorporated, 2005.
    [10]
    AUTODYN user's manual revision 4.3[M].Concord, California, USA:Century Dynamics Incorporated, 2003.
    [11]
    迟润强. 弹丸超高速撞击薄板碎片云建模研究[D]. 哈尔滨: 哈尔滨工业大学, 2010.

    CHI R Q.Research and modeling of debris cloud produced by hypervelocity impact of projectile with thin plate[D].Harbin:Harbin Institute of Technology, 2010.
    [12]
    LIU X, GAI F F, CHENG S.Numerical simulation on characteristics of debris clouds produced by conical projectiles hypervelocity impact on thin plates[J].Int J Hybrid Inf Technol, 2015, 8(6):79-86. doi: 10.14257/ijhit
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