空间飞行器总体设计的电磁兼容性问题

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空间飞行器总体设计的电磁兼容性问题

刘建新，唐泽群

北京邮电大学，北京空间飞行器总体设计部

发布日期:1996-04-25

ELECTROMAGNETIC COMPATIBILITY PROBLEMS IN SPACECRAFT SYSTEM DESIGN

Liu Jianxin; Tang Zequn(Beijing University of Posts and Telecommunications, Beijing 100088)(Beijing Institute of Spacecraft System Engineering, Beijing 100086)

Published:1996-04-25

摘要/Abstract

摘要： 结合空间飞行器总体设计的特点，介绍了电磁兼容性概念及其发展过程；分析了空间飞行器所处的电磁环境，指出总体设计中的若干电磁兼容性问题；提出了空间飞行器研制各阶段中开展电磁兼容性工作的流程图，强调必须在目前和今后各种型号的空间飞行器研制中引起充分的重视。

关键词: 航天器环境；电磁兼容性；程序框图；设计

Abstract: n this article, under the features of spacecraft system design, the EMC concept and its development are introduced. The electromagnetic environment of spacecraft is analyzed, and several EMC problems in spacecraft system design are pointed out. The content of EMC work during each phase of spacecraft development is put forward and it is emphasized that we must pay high attention to EMC of every sort of spacecraft.

刘建新，唐泽群. 空间飞行器总体设计的电磁兼容性问题[J]. .

Liu Jianxin; Tang Zequn(Beijing University of Posts and Telecommunications, Beijing 100088)(Beijing Institute of Spacecraft System Engineering, Beijing 100086). ELECTROMAGNETIC COMPATIBILITY PROBLEMS IN SPACECRAFT SYSTEM DESIGN[J]. .