首页> 外文期刊>IEEE Transactions on Plasma Science >Computer Simulations and Experimental Verification of the Nanoconductivity Concept for the Spacecraft Electronics
【24h】

Computer Simulations and Experimental Verification of the Nanoconductivity Concept for the Spacecraft Electronics

机译:航天器电子纳米导电性概念的计算机模拟和实验验证

获取原文
获取原文并翻译 | 示例

摘要

This paper develops the concept of the nanoconductivity of insulators as applied to the space technology aimed at creating discharge-free space vehicles and discusses the ways to achieve this. Feasibility analysis of advanced, next generation, discharge-free satellites widely using nanoconducting insulators in spacecraft electronics proves that such a transition is not only necessary but is also practicable. We have performed computer simulations of a multivibrator, which is a typical representative of the digital technology, using the LTspice software. As any spacecraft dielectric is a potential source of the electrostatic discharges, it is advisable to implement the nanoconductivity concept by replacing high-resistivity insulators with the nanoconducting dielectrics featuring electrical conductivity around .
机译:本文提出了绝缘子的纳米导电性的概念,并将其应用于旨在创建无放电空间飞行器的空间技术,并讨论了实现这一目标的方法。在航天器电子设备中广泛使用纳米导电绝缘子的先进的下一代无放电卫星的可行性分析证明,这种过渡不仅是必要的,而且也是可行的。我们已经使用LTspice软件对多谐振荡器进行了计算机仿真,这是数字技术的典型代表。由于任何航天器电介质都是静电放电的潜在来源,因此建议采用纳米电导率大约为1的纳米导电电介质来代替高电阻绝缘体,从而实现纳米电导率的概念。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号