首页 | 本学科首页   官方微博 | 高级检索  
     检索      

可重复使用热防护材料应用与研究进展
引用本文:黄红岩,苏力军,雷朝帅,李健,张恩爽,李文静,杨洁颖,赵英民,裴雨辰,张昊.可重复使用热防护材料应用与研究进展[J].航空学报,2020,41(12):23716-023716.
作者姓名:黄红岩  苏力军  雷朝帅  李健  张恩爽  李文静  杨洁颖  赵英民  裴雨辰  张昊
作者单位:航天特种材料及工艺技术研究所, 北京 100074
摘    要:可重复使用热防护系统是为高速重复使用飞行器而发展的关键性技术,涵盖了地球大气环境及非地球大气环境下的弹道式再入、高马赫数巡航等应用场景。根据现有高马赫数飞行器热防护现状,对高马赫数飞行器的主要热防护系统类型、特点和使用场景进行了简要介绍。在此基础上,结合国外里程碑式可重复使用飞行器(X-15、SR-71、航天飞机、X-33、X-37B、Spaceliner等),梳理了可重复使用热防护材料的应用与研究进展,论述了代表性可重复使用热防护材料的发展、性能、研制进度、特点及应用前景。对国外在可重复使用热防护材料研制中的设计及发展思路,以及所存在的主要问题进行了总结归纳,为可重复使用热防护材料未来的发展提供了思路。

关 键 词:可重复使用热防护系统  陶瓷基复合材料  金属热防护系统  热结构  可重复使用飞行器  
收稿时间:2019-12-09
修稿时间:2020-02-04

Reusable thermal protective materials:appl ication and research progress
HUANG Hongyan,SU Lijun,LEI Chaoshuai,LI Jian,ZHANG Enshuang,LI Wenjing,YANG Jieying,ZHAO Yingmin,PEI Yuchen,ZHANG Hao.Reusable thermal protective materials:appl ication and research progress[J].Acta Aeronautica et Astronautica Sinica,2020,41(12):23716-023716.
Authors:HUANG Hongyan  SU Lijun  LEI Chaoshuai  LI Jian  ZHANG Enshuang  LI Wenjing  YANG Jieying  ZHAO Yingmin  PEI Yuchen  ZHANG Hao
Institution:Aerospace Research Institute of Special Material and Processing Technology, Beijing 100074, China
Abstract:Reusable Thermal Protection Systems (TPS) are the key technology required for a range of high speed vehicles from ballistic reentry to hypersonic cruise vehicles, within either the Earth atmosphere or non-Earth atmospheres. The main types, characteristics, and the application environment of thermal protection systems for high speed vehicles are briefly summarized based on the status quo of thermal protection strategies for high speed vehicles. The application and research progress of the reusable thermal protection materials for foreign milestone Reusable Launch Vehicles (RLVs) (e.g. X-15, SR-71, Space shuttle, X-33, X-37B, Spaceliner) are further reviewed, the development, material properties, research progress, material characteristics and application prospect of representative reusable thermal protection materials are discussed, and the design and development ideas of the reusable thermal protection materials and the existing problems are summarized. The future development of the reusable thermal protection materials is finally discussed.
Keywords:reusable thermal protection systems  Ceramic Matrix Composites  metallic TPS  hot structure  Reusable Launch Vehicles (RLVs)  
本文献已被 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号