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可重复使用航天器耐高温复合材料结构设计技术OA北大核心CSTPCD

Design Technology Research of Heat-resistant Composites for Reusable Aerospace Vehicles Structure

中文摘要英文摘要

针对未来可重复使用航天器需求,本文首先简要分析了国外典型重复使用航天器耐高温复合材料结构设计技术应用进展与特点,包括美国X系列、追梦者飞行器.然后从结构选材、设计和分析等方面,论述了可重复使用航天器大量应用先进耐高温树脂基复合材料整体结构相关的主要工程技术现状和发展方向,从工程应用角度为未来可重复使用航天器结构研制提供理论分析.最后介绍了未来需开展的可重复使用航天器耐高温复合材料结构设计技术重点研究内容.

In response to the demand for future reusable spacecraft,this article first briefly analyzes the application progress and characteristics of heat-resistance composite structure design technology for typical reusable spacecraft abroad,including the American X series and the Dream Chaser spacecraft.Then,from the aspects of structural material selection,design and analysis,the current status and development direction of the main engineering technologies related to the large-scale application of advanced heat-resistant resin-based composite in the overall structure of reusable spacecraft is discussed,theoretical analysis for the future development of reusable spacecraft structures from an engineering application perspective is provided.Finally,the key research content of the heat-resistant composite structure design technology for future reusable spacecraft is introduced.

邓云飞;顾春辉;尹进;程锋;李丹圆;赵锐霞;孙宏杰

北京宇航系统工程研究所,北京 100076航天材料及工艺研究所,北京 100076

航天器复合材料结构设计耐高温

AspacecraftCompositeStructure designHeat-resistant

《宇航材料工艺》 2024 (002)

11-17 / 7

10.12044/j.issn.1007-2330.2024.02.002

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