Research on Thermal Protection Technologies for Manned Space Vehicles

机译：载人航天器热防护技术研究

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To develop the thermal protection technologies required for atmospheric re-entry vehicles, research has been performed on the erosion mechanism of carbon/carbon (C/C) composite materials. The erosion and oxidation phenomena of CVD (Chemical Vapor Deposition)-SiC thermal protection coatings are important factors in this respect. High purity CVD-SiC samples were selected to evaluate the phenomena by comparing them with those of the C/C materials. This paper describes the latest results.

机译：为了开发大气再进入车辆所需的热防护技术，已经对碳/碳（C / C）复合材料的腐蚀机理进行了研究。在这方面，CVD（化学气相沉积）-SiC热防护涂层的腐蚀和氧化现象是重要的因素。选择高纯度CVD-SiC样品，通过将其与C / C材料的现象进行比较来评估这种现象。本文介绍了最新结果。

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来源
《International Symposium on Beyond the International Space Station: the Future of Human Spaceflight Jun 4-7, 2002 Strasbourg, France》|2002年|p.317-318|共2页
会议地点 Strasbourg(FR)
作者
T.Yoshinaka; Y.Morino;
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作者单位

National Space Development Agency of Japan (NASDA), 2-1-1 Sengen, Tsukuba, Ibaraki 305-8505, Japan;

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会议组织
原文格式 PDF
正文语种 eng
中图分类航天（宇宙航行）;
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Research on Thermal Protection Technologies for Manned Space Vehicles

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