| 高超声速飞行器控制面热防护系统地面试验研究 |
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| 引用本文： | 王立研.高超声速飞行器控制面热防护系统地面试验研究[J].宇航材料工艺,2016,46(1). |
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| 作者姓名： | 王立研 |
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| 作者单位： | 北京航天长征飞行器研究所 |
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| 摘 要： | 针对高超声速飞行器控制面研发手段中极其重要的地面试验技术,以X-37轨道飞行器为例,介绍了国外的最新研究进展和关键技术解决途径,以及指导地面试验研究的方法,并针对控制面方案在评估和鉴定中必不可少的高温模态试验,进行了综述和分析。
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| 关 键 词： | 高超声速飞行器 控制面 地面试验 高温模态试验 |
Research on TPS Ground Test for Control Surface of Hypersonic Vehicles |
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| Institution: | Beijing Institute of Space Long March Vehicle |
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| Abstract: | Ground test plays a very importance role in developing the control surface of hypersonic vehicles.This paper introduces the latest technical progress of ground test, solutions to critical technology and methodologyguiding the ground test by taking X-37 orbital vehicle as an example. And then, it summarizes the high-temperaturemodal survey of a hot structure control surface, which is an essential part in evaluating the control surface concept. |
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| Keywords: | Hypersonic vehicles Control surface Ground test High-temperature modal test |
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