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低地球軌道航天器對接放電研究

Discharging during LEO spacecraft docking

  • 摘要: 文章介紹了低軌道航天器對接放電的產(chǎn)生機(jī)理,通過模擬試驗(yàn)、電路仿真和理論分析,研究了低軌道航天器對接產(chǎn)生靜電放電的可能性、條件、放電強(qiáng)度、持續(xù)時間及其影響,并提出防止靜電放電危害的措施,為工程應(yīng)用提出參考建議。

     

    Abstract: This paper studies the discharging mechanism during low-orbit spacecraft docking, by using a set of experimental devices for simulating spacecraft docking charging and discharging. The experimental study, circuit simulation and theoretical analysis reveal the possibility, conditions, discharge intensity, duration and impact of electrostatic discharge when two low-orbit spacecrafts mate with each other. Some measures are proposed to prevent electrostatic discharge hazards in engineering applications.

     

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