| 注册
首页|期刊导航|宇航材料工艺|多层隔热结构研究进展

多层隔热结构研究进展

赵一搏 杨汝平 邱日尧 马晓静 许小强

宇航材料工艺2013,Vol.43Issue(4):29-34,6.
宇航材料工艺2013,Vol.43Issue(4):29-34,6.

多层隔热结构研究进展

Recent Progress on Multi-Layer Insulation Structures

赵一搏 1杨汝平 1邱日尧 1马晓静 1许小强1

作者信息

  • 1. 航天材料及工艺研究所,北京100076
  • 折叠

摘要

Abstract

Multi-layer insulation structures (MLI) are a kind of composite mostly used as thermal insulation of the aerocraft and propellant tank in the space.In this paper,heat insulating principle,composition,processing technology and the application of MLI are reviewed.The recent the progress and tendency of MLI is introduced briefly.With the purpose of landing on moon and deep space exploration,the property of MLI must be improved.

关键词

运载火箭/燃料贮箱/多层隔热

Key words

Launch vehicle/ Propellant tank/ Multi-layer insulation

引用本文复制引用

赵一搏,杨汝平,邱日尧,马晓静,许小强..多层隔热结构研究进展[J].宇航材料工艺,2013,43(4):29-34,6.

宇航材料工艺

OA北大核心CSCDCSTPCD

1007-2330

访问量0
|
下载量0
段落导航相关论文