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一、前言菊3号卫星是日本研制的第一颗大型人造卫星,1981年2月从种子岛宇宙中心发射。菊3号的设计要求是各分系统从研制到生产的各个阶段都能满足预期的功能和性能,而且要求卫星与新火箭和地面装置间具有相容性。1980年夏证实了初样星和地面试验用火箭(GTV)间的相容性,1981年5月,飞行卫星结束了所执行的实验使命。之所以能做到这一点,其重要因素可归结为对电磁相容性的管理。本文概述了与电磁相容性(EMC)有关的分析和试验概况。
I. Introduction Chrysanthemum 3 was the first large-scale satellite manufactured by Japan and launched from the Seed Island Cosmos Center in February 1981. The design requirements for the No. 3 chrysanthemum are that all subsystems of the subsystem can meet the expected functions and performance from development to production and that the compatibility of satellites with the new rockets and ground devices is required. The summer of 1980 confirmed the compatibility of the nascent prototype with the ground-based experimental rocket (GTV). In May 1981, the flying satellite concluded its experimental mission. The key reason for this can be attributed to the management of electromagnetic compatibility. This article provides an overview of the analytical and experimental aspects related to electromagnetic compatibility (EMC).