本标准提供了在地球电离层中运行高压系统时可能产生的各种等离子体相互作用的相关要求，以及消除或减轻此类反应的标准实践。本标准的目的是为高压空间电力系统（>55伏）（V））提供一个设计标准，该系统在与低地球轨道（海拔200至1000公里，纬度在-50至+50度）相关的等离子体环境中运行。这种电力系统，尤其是太阳能电池板，是低轨航天器充电的直接原因； 这些系统可以以多种方式与这个环境交互，这对它们自身以及部署它们的平台或车辆都有潜在的破坏性。美国国家航空航天局认可。奥西。

This standard provides requirements relative to various plasma interactions that can result when a high-voltage system is operated in the Earth's ionosphere and standard practices to eliminate or mitigate such reactions. The purpose of this standard is to provide a design standard for high-voltage space power systems (> 55 volts) (V))that operate in the plasma environment associated with LEO (altitude from 200 and 1000 km and latitude between -50 and +50 degrees). Such power systems, particularly solar arrays, are the proximate cause of spacecraft charging in LEO; and these systems can interact with this environment in a number of ways that are potentially destructive to themselves as well as to the platform or vehicle that has deployed them. NASA Endorsed. OCE.