Engineering Methodology for the Selection of a Composite Polymer Dielectric that Ensures the Absence of Electrostatic Discharges in the Design of the Onboard Electronic Equipment of the Spacecraft

Dmitrii Abrameshin, S. Tumkovskiy, V. Saenko, E. Pozhidaev
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Abstract

an engineering technique for selecting a composite polymer dielectric with increased conductivity, ensuring the absence of electrostatic discharges, has been developed for radio electronic devices as part of the onboard equipment of spacecraft. On the basis of the developed methodology, at the stages of preliminary and technical design, calculations of the operability of the developed radioelectronic means are carried out in relation to the invariability of the operating characteristics specified according to the terms of reference, and at the same time there is no electrostatic discharges of the printed circuit board substrate - printed conductor. The method is based on comparison of the conductivity value of the composite dielectric of the printed circuit board of the developed radio-electronic apparatuses, at which its operating parameters are still unchanged, with the criterion conductivity value ensuring the absence of electrostatic discharges –10-9 Ω-1 ·m-1. The method is intended for the developed avionics of space application, operating on board the spacecraft, operated in conditions of intense impact of space plasma.
航天器机载电子设备中保证无静电放电的复合聚合物电介质选择的工程方法
针对航天器机载无线电电子器件,提出了一种提高电导率、保证无静电放电的复合聚合物电介质选择工程技术。在开发的方法的基础上,在初步和技术设计阶段,根据参考条款规定的工作特性的不变性,对开发的无线电电子设备的可操作性进行了计算,同时印刷电路板衬底-印刷导体没有静电放电。该方法是将研制的无线电电子设备印刷电路板的复合介质在其工作参数不变的情况下的电导率值与保证无静电放电的准则电导率值-10-9 Ω-1·m-1进行比较。该方法适用于在空间等离子体强烈冲击条件下,在航天器上运行的先进的空间应用航空电子设备。
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