中国空间科学技术

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热管辐射器设计、试验及其在通信广播卫星上的应用

华诚生   

  1. 北京空间飞行器总体设计部
  • 发布日期:1995-06-25

DESIGN,TEST OF SPACECRAFT HEAT PIPE RADIATOR AND ITS APPLICATION FOR COMMUNICATION AND BROADCASTING SATELLITE

Hua Chengsheng(Beijing Institute of Spacecraft System Engineering, Beijing 100086)   

  • Published:1995-06-25

摘要： 首先介绍了热管辐射器的计算及优化设计的理论。制作了两个铝蜂窝板热管辐射器单元试件，一个是热管预埋的，一个是热管外贴的。通过试验比较了这两种形式辐射器，并验证了理论计算。还介绍了用于广播通信卫星行波管散热用热管辐射器的设计及太阳模拟热平衡试验结果。

关键词: 热管, 辐射器, 设计, 实验, 分析, 通信卫星

Abstract: This paper describes the method of the thermal analysis and optimization design for spacecraft heat pipe radiator.Two test samples of aluminium honeycomb heat pipe racliaror were built.In one of the samples the heat Pipes are inserted into the honeycomb panel facesheets and in the other the heat pipes are installed on the facesheet.Thermal performance of the two type radiators were evaluated by the tests and the theroretical calculation was proved.The design and solar simulation test of a heat pipe radiator for cooling TWTA of communication and Broadcating satellite are presented.