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航天器热试验外热流实施和测试探索
引用本文:邵兴国,刘自军,谭沧海,向艳超.航天器热试验外热流实施和测试探索[J].航天器工程,2007,16(4):94-98.
作者姓名:邵兴国  刘自军  谭沧海  向艳超
作者单位:北京空间飞行器总体设计部,北京,100094
摘    要:介绍了空间探测卫星热平衡试验的外热流设计和测试方案,热试验中共采用了5种热流计,试验前进行了单体标定和等效热环境标定,测试到了红外灯功率与热流计温度响应特性。为准确验证卫星的温度特性,试验设计了瞬态外热流试验。绝热型热流计在热平衡试验中为控制热流计。

关 键 词:热平衡试验  热流测试  热流计标定
文章编号:1673-8748(2007)04-0094-05
修稿时间:2007年1月26日

Research on Heat Flux Measurement and Simulation in Thermal Balance Test of Spacecraft
SHAO Xingguo,LIU Zijun,TAN Canghai,XIANG Yanchao.Research on Heat Flux Measurement and Simulation in Thermal Balance Test of Spacecraft[J].Spacecraft Engineering,2007,16(4):94-98.
Authors:SHAO Xingguo  LIU Zijun  TAN Canghai  XIANG Yanchao
Abstract:The heat flux measurement method and simulation was illustrated in this paper used in thermal balance test(TBT)of CHANG'E lunar satellite,in which five kinds of radiometers were used.The calibration of the radiometers was undertaken respectively in the separate states and simulated environmental conditions.The response characteristics were given under different heat flux condition.As the characteristic of temperature distribution must be validated,the transient heat flux state was designed during TBT.The thermal insulation radiometers were used as a controling radiometer mainly action in TBT.
Keywords:thermal balance test  heat flux measurement  radiometer calibartion
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