摘要
在微波雷达成像卫星的整星真空热试验中,需采取特殊措施吸收SAR天线T/R组件发射出的大功率微波,以保护组件不被损伤。文章介绍了一种新型外热流模拟装置——吸波热沉,兼具吸波和外热流模拟2方面的功能。为验证吸波热沉在真空热试验时的有效性,设计了一套验证试验方案,试验结果表明:吸波热沉可以满足真空热试验的外热流模拟精度需求,偏差在4%以内。该装置已在某微波雷达成像卫星的真空热试验中成功应用。
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.
出处
《航天器环境工程》
2017年第5期505-509,共5页
Spacecraft Environment Engineering
基金
国家重大科技专项工程
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
microwave radar imaging satellite
SAR antenna
thermal vacuum test
microwave absorbing heat sink
external heat flux simulation
temperature control