刘海波, 李得天, 杨生胜, 等. 不同面积Kapton材料的放电特性实验研究[J]. 真空与低温, 2014, 20(3): 140-144. DOI: 10.3969/j.issn.1006-7086.2014.03.004
引用本文: 刘海波, 李得天, 杨生胜, 等. 不同面积Kapton材料的放电特性实验研究[J]. 真空与低温, 2014, 20(3): 140-144. DOI: 10.3969/j.issn.1006-7086.2014.03.004
LIU Hai-bo, LI De-tian, YANG Sheng-sheng, et al. DISCHARGE CHARACTERISTICS EXPERIMENT RESEARCH ON DIFFERENT AREA OF KAPTON MATERIAL[J]. VACUUM AND CRYOGENICS, 2014, 20(3): 140-144. DOI: 10.3969/j.issn.1006-7086.2014.03.004
Citation: LIU Hai-bo, LI De-tian, YANG Sheng-sheng, et al. DISCHARGE CHARACTERISTICS EXPERIMENT RESEARCH ON DIFFERENT AREA OF KAPTON MATERIAL[J]. VACUUM AND CRYOGENICS, 2014, 20(3): 140-144. DOI: 10.3969/j.issn.1006-7086.2014.03.004

不同面积Kapton材料的放电特性实验研究

DISCHARGE CHARACTERISTICS EXPERIMENT RESEARCH ON DIFFERENT AREA OF KAPTON MATERIAL

  • 摘要: 航天器表面介质材料在空间等离子环境下会产生放电现象,放电诱发的瞬态脉冲会对航天器在轨安全运行产生严重影响。通过对不同面积的125 μm厚Kapton温控材料进行放电实验,对放电诱发的瞬态脉冲进行测量,总结分析其规律,得出4~36 cm2 Kapton材料和64~225 cm2 Kapton材料的放电波形存在比较大的差异,而且随着材料面积增加,Kapton材料的放电电流峰值、放电持续时间、放电电荷损失量和放电频率都相应的升高。对Kapton材料放电特性的研究,将为航天器带电防护设计和放电危害评估提供数据支持。

     

    Abstract: Spacecraft surface materials will discharge in the space plasma environment.The discharge induced transient pulse can cause serious problems to the safety and reliability of spacecraft. Through the discharge experiment of 125 μm Kapton temperature control material of different areas, Measurement of discharge induced transient pulse and analysis of its law, results show that the discharge waveform of the 4~36 cm2 Kapton material and the 64~225 cm2 Kapton materials appear relatively large differences, and with the increasing material area, discharge peak current, discharge pulse duration, discharge released charge and the discharge frequency increase accordingly. Through the research on the discharge characteristics of Kapton materials, to provide data support for the spacecraft charging protection and discharge hazard assessment.

     

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