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吸波热沉在微波雷达成像卫星真空热试验中的应用

胡小康 翟载腾 程锋 史奇良 葛钊

航天器环境工程2017,Vol.34Issue(5):505-509,5.
航天器环境工程2017,Vol.34Issue(5):505-509,5.DOI:10.3969/j.issn.1673-1379.2017.05.009

吸波热沉在微波雷达成像卫星真空热试验中的应用

Application of microwave absorbing heat sink in the thermal vacuum test of microwave radar imaging satellite

胡小康 1翟载腾 1程锋 1史奇良 1葛钊1

作者信息

  • 1. 上海卫星工程研究所,上海 201109
  • 折叠

摘要

Abstract

In the vacuum thermal test for the SAR satellite, special measures should be taken to absorb the high power microwave emitted by the transmitter-receiver subassembly to protect it from damage. This paper introduces a new heat flux simulation device, with the functions of both absorbing the wave and simulating the heat flux. In order to verify the validity of the microwave absorbing heat sink, a calibration experiment is carried out. The experimental results show that the heat sink can meet the requirements of external flux precision for the thermal vacuum test, with a bias not more than 4%. The heat sink has been successfully applied in the thermal vacuum test of a SAR satellite.

关键词

微波雷达成像卫星/SAR天线/真空热试验/吸波热沉/外热流模拟/温度控制

Key words

microwave radar imaging satellite/SAR antenna/thermal vacuum test/microwave absorbing heat sink/external heat flux simulation/temperature control

分类

航空航天

引用本文复制引用

胡小康,翟载腾,程锋,史奇良,葛钊..吸波热沉在微波雷达成像卫星真空热试验中的应用[J].航天器环境工程,2017,34(5):505-509,5.

基金项目

国家重大科技专项工程 ()

航天器环境工程

OACSTPCD

1673-1379

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