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红外加热棒式外热流模拟器在航天器真空热试验中的性能分析
引用本文:柳晓宁,郭鹏,申彬,曹志松. 红外加热棒式外热流模拟器在航天器真空热试验中的性能分析[J]. 航天器环境工程, 2015, 32(4): 419-423
作者姓名:柳晓宁  郭鹏  申彬  曹志松
作者单位:1. 北京卫星环境工程研究所;2. 可靠性与环境工程技术重点实验室, 北京 100094
摘    要:基于红外加热棒的稳态传热特性,建立了红外加热棒式外热流模拟器的计算模型,对其加热能力及效果进行计算分析。以实际红外加热棒式外热流模拟器为对象开展了试验验证,对模拟器的温度响应特点、加热能力进行了全面测试。结果表明,该种红外模拟器温度响应速度快,加热棒覆盖率、阻值可调整范围大,使得其加热能力设计灵活度高,能够适应航天器真空热试验的使用需求。

关 键 词:红外加热棒  外热流模拟器  有限元分析  热真空试验
收稿时间:2015-01-16
修稿时间:2015-07-15

The external-heat simulator with infrared heating rod for spacecraft thermal vacuum tests
Liu Xiaoning,Guo Peng,Shen Bin,Cao Zhisong. The external-heat simulator with infrared heating rod for spacecraft thermal vacuum tests[J]. Spacecraft Environment Engineering, 2015, 32(4): 419-423
Authors:Liu Xiaoning  Guo Peng  Shen Bin  Cao Zhisong
Affiliation:1. Beijing Institute of Spacecraft Environment Engineering;2. Science and Technology on Reliability and Environmental Engineering Laboratory, Beijing 100094, China
Abstract:The theory and the numerical analysis of the external-heat simulator with infrared heating rod are discussed, together with its applications in the thermal vacuum tests. The computational model of the new external-heat simulator is built to analyze its heating capability and the temperature control effect. Tests are carried out to validate the temperature response characteristics and the heating capability of the simulator. The new simulator can be applied in the spacecraft thermal vacuum test, for its fast temperature response, the large range of the heating rod coverage coefficient and resistance, which improves the flexibility of the heating capacity design.
Keywords:infrared heating rod  external-heat simulator  finite element analysis  thermal vacuum test
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