Study on the trap properties of nano-ZnO modified polyimide based on surface potential decay method

Bo Zhang, Jiang Wu, Xiaoquan Zheng
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Abstract

The space environment will charge the surface of the spacecraft. Due to the low discharge ability of the dielectric material, it may cause the surface discharge of the spacecraft and affect the normal work of the spacecraft. Polyimide is a typical dielectric material on the spacecraft, this paper attempts to improve the surface discharge ability by modifying polyimide with nano-ZnO. The research method is based on the surface potential decay platform, which is an intuitive approach to evaluate the states of surface charging. The surface potential decay characteristics of pure polyimide and its modified samples are tested. The surface potential decay mechanism of the dielectric is analyzed by calculating the trap characteristics. Results show that the surface potential of ZnO modified polyimide has less decrement and rate of decay than that of the pure polyimide. The deep trap density of electron trap and hole trap density is less than that of pure polyimide, the shallow trap of pure polyimide is the lowest. The change of electron trap level is small, while the hole trap level increases.
基于表面电位衰减法的纳米zno修饰聚酰亚胺的阱特性研究
空间环境会对航天器表面产生电荷。由于介质材料的放电能力较低,可能造成航天器表面放电,影响航天器的正常工作。聚酰亚胺是航天器上典型的介电材料,本文尝试用纳米氧化锌修饰聚酰亚胺,提高其表面放电能力。该研究方法基于表面电位衰减平台,是一种直观评价表面充电状态的方法。测试了纯聚酰亚胺及其改性样品的表面电位衰减特性。通过计算陷阱特性,分析了电介质的表面电位衰减机理。结果表明,ZnO改性聚酰亚胺的表面电位衰减幅度和衰减速率均小于纯聚酰亚胺。电子阱的深阱密度和空穴阱密度小于纯聚酰亚胺,纯聚酰亚胺的浅阱密度最低。电子阱能级变化不大,空穴阱能级增加。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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