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相控阵天线热真空试验控温方法

房澎涛 王升 孟通 刘捷 田维刚 黄睿 秦臻 徐新华

航天器环境工程2024,Vol.41Issue(2):190-194,5.
航天器环境工程2024,Vol.41Issue(2):190-194,5.DOI:10.12126/see.2023022

相控阵天线热真空试验控温方法

Method for temperature control of phased array antenna in thermal vacuum test

房澎涛 1王升 1孟通 1刘捷 1田维刚 1黄睿 1秦臻 1徐新华1

作者信息

  • 1. 中国空间技术研究院西安分院,西安 710000
  • 折叠

摘要

Abstract

In the thermal vacuum test of the phased array antenna,the heat dissipation radiator does not take part in the test.To ensure the temperature consistency of the phased array antenna between in the ground thermal vacuum test and in-orbit flight,a temperature control method was proposed by using a liquid cooling plate combined with a radiant heat sink and a conductive heat sink in vacuum chamber.The thermal vacuum test results show that the phased array antenna exhibits good temperature control state.The temperature fluctuation is±0.8℃,which meets the requirement of less than 2℃.The proposed method achieves the purpose of ground thermal vacuum test.

关键词

相控阵天线/热真空试验/热控设计/液冷板

Key words

phased-array antenna/thermal vacuum test/thermal control design/liquid cooling plate

分类

航空航天

引用本文复制引用

房澎涛,王升,孟通,刘捷,田维刚,黄睿,秦臻,徐新华..相控阵天线热真空试验控温方法[J].航天器环境工程,2024,41(2):190-194,5.

基金项目

国家自然科学基金项目(编号:62271387) (编号:62271387)

航天器环境工程

OACSTPCD

1673-1379

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