宇航材料工艺2013，Vol.43Issue(1)：20-25,6.
飞行器典型热密封结构
Typical High-Temperature Seal Structur of Reusable and Hypersonic Vehicles
李凡 1王树浩 2陈江涛 1赵光辉 2于焕光1
作者信息
- 1. 航天材料及工艺研究所,北京 100076
- 2. 二炮驻首都航天机械公司军事代表室,北京 100076
- 折叠
摘要
Abstract
Reusable and hypersonic vehicles pose an extraordinary challenge for seal structures. Airframes and engines require lightweight, high-temperature seal structural that can withstand the extreme environment of hypersonic flight. This paper reviews relevant seal technology for typical vehicles (e. g. Space Shuttle, X-38 and X-51) and presents several seal technologies for future hypersonic vehicles, foucs on high-temperature seal structural of the space shuttle TPS, vehicle penetrations and control surfaces.关键词
可重复使用飞行器/高超声速飞行器/热密封/密封结构Key words
Reusable vehicles/Hypersonic vehicles/High-temperature seal/Seal structural引用本文复制引用
李凡,王树浩,陈江涛,赵光辉,于焕光..飞行器典型热密封结构[J].宇航材料工艺,2013,43(1):20-25,6.
