| 返回式卫星主动段热控设计 |
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| 引用本文： | 李希伦.返回式卫星主动段热控设计[J].中国空间科学技术,1991,11(4):67-71. |
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| 作者姓名： | 李希伦 |
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| 作者单位： | 北京空间飞行器总体设计部 |
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| 摘 要： | 我国的一种返回式卫星发射时未设整流罩,星体直接受到气动加热。利用热惯性法进行主动段热控设计,理论计算值、试验值均未超过飞行测量数据,说明设计和计算是合理的。
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| 关 键 词： | 气动加热 卫星温度 热分析 |
THERMAL CONTROL DESIGN OF RETURNABLE SATELLITE IN LAUNCHING PHASE |
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| Li XiLun.THERMAL CONTROL DESIGN OF RETURNABLE SATELLITE IN LAUNCHING PHASE[J].Chinese Space Science and Technology,1991,11(4):67-71. |
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| Authors: | Li XiLun |
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| Institution: | Beijing Institute of Spacecraft Systems Engineering |
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| Abstract: | This paper discusses the problem of aerodynamics heat of non-fairinged satellite.The method of heat-inertia in launching phase,is usedin thermal control design.The theoretical data,test data and flight data are identical with eachother.It shows that the design is very successful. |
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| Keywords: | Aerodynamic heating Satellite temperature Thermal analysis Calculation |
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