AEROSPACE SHANGHAI, Volume. 41, Issue 5, 11(2024)

China Response to Risk of NEA and Kinetic Energy Impact Deflection Researches:Retrospect and Prospect

Zizheng GONG*... Guangming SONG, Chuan CHEN, Pinliang ZHANG, Wenjin LIU, Qingming ZHANG and Renrong LONG |Show fewer author(s)
Author Affiliations
  • Beijing Institute of Spacecraft Environment Engineering,Beijing100094,China
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    Figures & Tables(18)
    The near earth object survey and positioning system
    The active defense system composition
    The kinetic impact on asteroids
    Experimental system for momentum transfer characteristics of kinetic impact on asteroids
    Crater morphology of simulated asteroid samples[53-54]
    The relationship between pit depth,pit diameter,and impact velocity
    The relationship between the mass of the ejected object,β and the impact velocity
    Simplified calculation model for hypervelocity impact[54]
    Simulation results of experiment No.1
    The influence of impactor shape on momentum transfer coefficient
    The influence of impactor density on momentum transfer coefficient
    The influence of asteroid strength and porosity on momentum transfer coefficient
    The impact zone zoning for kinetic impact on asteroids
    The influence of impact position on the change in velocity of asteroids
    The main stages of mission implementation
    • Table 1. Physical and mechanical properties of asteroid simulation targets

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      Table 1. Physical and mechanical properties of asteroid simulation targets

      材料

      密度ρdry/

      (g.cm-3)

      孔隙率/%抗压强度/MPa抗拉强度/MPa
      玄武岩2.884~0144.59.83
    • Table 2. Comparison between experimental and simulation results

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      Table 2. Comparison between experimental and simulation results

      编号撞击速度/(km.s-1成坑直径成坑深度动量传递系数β
      实验/mm模拟/mm偏差/%实验/mm模拟/mm偏差/%实验模拟偏差/%
      13.9052487.71211.26.72.392.294.2
      26.30554714.513.5143.72.512.413.9
    • Table 3. The main parameters of three geometric shape impactors

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      Table 3. The main parameters of three geometric shape impactors

      弹丸形状尺寸/m质量/kg
      球形半径r=0.36515.33
      圆盘半径r=0.72 高h=0.144653.13
      圆柱半径r=0.36 高h=0.504571.49
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    Zizheng GONG, Guangming SONG, Chuan CHEN, Pinliang ZHANG, Wenjin LIU, Qingming ZHANG, Renrong LONG. China Response to Risk of NEA and Kinetic Energy Impact Deflection Researches:Retrospect and Prospect[J]. AEROSPACE SHANGHAI, 2024, 41(5): 11

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    Paper Information

    Category: Special Paper of Expert

    Received: Jul. 18, 2024

    Accepted: --

    Published Online: Jan. 15, 2025

    The Author Email:

    DOI:10.19328/j.cnki.2096-8655.2024.05.002

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