宇航材料工艺2024，Vol.54Issue(2)：11-17,7.DOI:10.12044/j.issn.1007-2330.2024.02.002
可重复使用航天器耐高温复合材料结构设计技术
Design Technology Research of Heat-resistant Composites for Reusable Aerospace Vehicles Structure
邓云飞 1顾春辉 1尹进 1程锋 1李丹圆 1赵锐霞 2孙宏杰2
作者信息
- 1. 北京宇航系统工程研究所,北京 100076
- 2. 航天材料及工艺研究所,北京 100076
- 折叠
摘要
Abstract
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.关键词
航天器/复合材料/结构设计/耐高温Key words
Aspacecraft/Composite/Structure design/Heat-resistant分类
通用工业技术引用本文复制引用
邓云飞,顾春辉,尹进,程锋,李丹圆,赵锐霞,孙宏杰..可重复使用航天器耐高温复合材料结构设计技术[J].宇航材料工艺,2024,54(2):11-17,7.
