| 纯辐射换热航天器系统比缩热负载试验方法 |
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| 引用本文： | 李大耀,李大治.纯辐射换热航天器系统比缩热负载试验方法[J].中国空间科学技术,1993,13(6):16-21. |
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| 作者姓名： | 李大耀 李大治 |
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| 作者单位： | 北京空间机电研究所
(李大耀)，南通医学院(李大治) |
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| 摘 要： | 首先讨论了纯辐射换热的航天器系统温度场在恒定热源情况下具有渐近稳定特性，然后据此提出了对该系统可采用比缩热负载进行热模拟试验的方法。
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| 关 键 词： | 热辐射 航天器 热模拟 研究 |
EXPERIMENTAL METHOD OF HEAT ANALOGY USING REDUCED HEAT LOAD FOR RADIATIVE THERMAL EXCHANGE SPACECRAFT SYSTEM |
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| Li Dayao.EXPERIMENTAL METHOD OF HEAT ANALOGY USING REDUCED HEAT LOAD FOR RADIATIVE THERMAL EXCHANGE SPACECRAFT SYSTEM[J].Chinese Space Science and Technology,1993,13(6):16-21. |
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| Authors: | Li Dayao |
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| Institution: | Li Dayao (Beijing Institute of Space Machine and Electricity)
Li Dazhi (Nantong Medical College) |
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| Abstract: | The asymptotical characteristic of temperature field for theradiative thermal exchange spacecraft system in the condition of constantheat sources is discussed first.Then,according this result,the experi-mental method of heat analogy that uses the reduced heat load for abovesystem is given. |
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| Keywords: | Thermal radiation Spacecraft Thermal simulation Research |
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