Shock Initiation of a Satellite Tank under Debris Hypervelocity Impact

被引:5
|
作者
Zhao, Beilei [1 ]
Zhao, Jiguang [2 ]
Cui, Cunyan [1 ]
Wang, Yan [1 ]
机构
[1] Space Engn Univ, Dept Aerosp Sci & Technol, Beijing 101416, Peoples R China
[2] Space Engn Univ, Dept Elect & Opt Engn, Beijing 101416, Peoples R China
来源
APPLIED SCIENCES-BASEL | 2019年 / 9卷 / 19期
关键词
shock initiation; satellite tank; debris; hypervelocity impact; numerical simulation;
D O I
10.3390/app9193957
中图分类号
O6 [化学];
学科分类号
0703 ;
摘要
Featured Application The initiation criterion for the liquid hydrazine tank and numerical simulation developed in this paper can be used to determine whether the satellite tank explodes under the debris hypervelocity impact, which is of great significance for the damage consequence analysis and risk assessment of the satellite. Abstract For the risk assessment of a satellite to determine whether the satellite tank explodes under the hypervelocity impact, the Walker-Wasley criterion is selected to predict the shock initiation of the satellite tank. Then, the minimum power density of liquid hydrazine is determined based on the tests, the expressions of shock wave pressure and pressure duration are constructed based on the one-dimensional wave theory, and the initiation criterion for the liquid hydrazine tank is established. Finally, numerical simulation and the initiation criterion are adopted to calculate the power density in the satellite tank under the debris impact at the velocity of 10 km/s. The calculated power density agrees well with the simulated power density, they are both larger than the minimum power density, demonstrating that the shock wave generated by the hypervelocity impact is sufficient to trigger an explosion in the satellite tank.
引用
收藏
页数:16
相关论文
共 50 条
  • [1] Hydrodynamic Ram Effect Caused by Debris Hypervelocity Impact on Satellite Tank
    Zhao, Beilei
    Zhao, Jiguang
    Cui, Cunyan
    Duan, Yongsheng
    [J]. APPLIED SCIENCES-BASEL, 2019, 9 (20):
  • [2] Debris area distribution of spacecraft under hypervelocity impact
    Lan, Sheng-wei
    Liu, Sen
    Li, Yi
    Ke, Fa-wei
    Huang, Jie
    [J]. ACTA ASTRONAUTICA, 2014, 105 (01) : 75 - 81
  • [3] Composite Materials Behavior Under Hypervelocity Debris Impact
    Katz, S.
    Grossman, E.
    Gouzman, I.
    Murat, M.
    Wiesel, E.
    Wagner, H. D.
    [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 2009, 46 (02) : 230 - 235
  • [4] OTM analysis of debris cloud under hypervelocity impact
    Liao, Huming
    Li, Bo
    Fan, Jiang
    Jiao, Lixin
    Yu, Shuaichao
    Lin, Jianyu
    Pei, Xiaoyang
    [J]. Baozha Yu Chongji/Explosion and Shock Waves, 2022, 42 (10):
  • [5] Fracture initiation mechanisms in α-alumina under hypervelocity impact
    Zhang, Cheng
    Kalia, Rajiv K.
    Nakano, Aiichiro
    Vashishta, Priya
    [J]. APPLIED PHYSICS LETTERS, 2007, 91 (12)
  • [6] High pressure composite tank behaviour under an hypervelocity impact
    Salome, R
    Albouys, V
    Le Floc'h, C
    Sornette, D
    Vila, JP
    [J]. PROCEEDINGS OF THE THIRD EUROPEAN CONFERENCE ON SPACE DEBRIS, VOLS 1 AND 2, 2001, 473 : 621 - 627
  • [7] Debris analysis of on-orbit satellite collision based on hypervelocity impact simulation
    Zhang, Xiaotian
    Jia, Guanghui
    Huang, Hai
    [J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2011, 32 (07): : 1224 - 1230
  • [8] CHARACTERISTICS OF HYPERVELOCITY IMPACT DEBRIS CLOUDS
    KLOPP, RW
    SHOCKEY, DA
    OSHER, JE
    CHAU, HH
    [J]. INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1990, 10 (1-4) : 323 - 335
  • [9] A new breakup threshold model for satellite under hypervelocity impact
    Li, Yi
    Huang, Jie
    Ma, Zhao-Xia
    Lan, Sheng-Wei
    Liu, Sen
    [J]. Yuhang Xuebao/Journal of Astronautics, 2012, 33 (08): : 1158 - 1163
  • [10] Numerical simulation of shock initiation of confined charge by debris impact
    Zhou, Shuang
    Chen, Li
    Zhang, Qing-Ming
    [J]. Binggong Xuebao/Acta Armamentarii, 2015, 36 : 317 - 321