摘要
文章基于电磁监测卫星的空间等离子体表面带电环境和等电位要求,对卫星多层隔热组件表面等电位的控制方法进行分析和优化,给出多层隔热组件制作、安装、接地、检测和保护工艺方法,从而满足整星表面的电位差在±2 V以内的控制要求。
This paper analyzes and optimizes the method of equipotential control on the surface of the multilayer heat insulation of an electromagnetic monitoring satellite in the space plasma charging environment of the satellite and with consideration of its surface equipotential requirements. The desirable working processes for the multilayer components are proposed, including the fabrication, the installation, the grounding, the detection, and the protection, to meet the requirement of controlling the surface potential difference of the whole satellite within ±2 V.
作者
左颖萍
周传君
朱兴鸿
范庆梅
ZUO Yingping;ZHOU Chuanjun;ZHU Xinghong;FAN Qingmei(DFH Satellite Co., Ltd, Beijing 100094, China)
出处
《航天器环境工程》
2018年第2期195-199,共5页
Spacecraft Environment Engineering
关键词
电磁监测卫星
多层隔热组件
空间等离子体环境
表面带电
等电位控制
接地
electro-magnetic monitoring satellite
multilayer insulation
space plasma environment
surface charging
equipotential control
grounding