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高速柔性气动减速器关键技术研究进展

薛晓鹏 贾贺 荣伟 蒋伟 包文龙 王臻 邹天琪 代雨柔 周一苇

航空学报2025,Vol.46Issue(1):1-31,31.
航空学报2025,Vol.46Issue(1):1-31,31.DOI:10.7527/S1000-6893.2025.31677

高速柔性气动减速器关键技术研究进展

Review of high-speed flexible aerodynamic decelerators key technologies

薛晓鹏 1贾贺 2荣伟 2蒋伟 2包文龙 2王臻 2邹天琪 2代雨柔 2周一苇1

作者信息

  • 1. 中南大学 自动化学院,长沙 410083
  • 2. 北京空间机电研究所,北京 100094
  • 折叠

摘要

Abstract

Flexible aerodynamic deceleration technology is extremely key for spacecraft to safely land in extraterres-trial objects or re-enter the Earth's atmosphere at high speeds.With the continuous advancement of major missions such as Chinese manned spaceflight and deep space exploration,the demand for high-speed flexible aerodynamic de-celerator for spacecraft with faster entry speeds and heavier loads is becoming increasingly urgent.However,the me-chanical model of high-speed flexible aerodynamic decelerator combines strong nonlinearity and strong coupling char-acteristics,and involves a wide range of research fields,such as the aerodynamic characteristics of blunt and porous structures,nonlinear structural dynamics,compressible turbulence,structural aerodynamic heat and their mutual cou-pling issues.Therefore,conducting research on the fundamental theory and key technologies of flexible aerodynamic decelerators is of great difficulty and complexity,but of great significance.This paper,first,classifies the high-speed flexible aerodynamic decelerators.Then,the technical content of high-speed flexible aerodynamic decelerator technol-ogy is analyzed and sorted out,and the development history and research progress of its key technologies are system-atically reviewed and summarized.Finally,a summary and outlook are provided on the future development directions and key issues that urgently need to be addressed for the key technologies of high-speed flexible aerodynamic decelerators.

关键词

进入减速着陆/超声速降落伞/充气式进入减速器/气动特性/流固热耦合

Key words

entry,descent and landing/supersonic parachute/inflatable entry decelerator/aerodynamic character-istic/fluid solid thermal coupling

分类

航空航天

引用本文复制引用

薛晓鹏,贾贺,荣伟,蒋伟,包文龙,王臻,邹天琪,代雨柔,周一苇..高速柔性气动减速器关键技术研究进展[J].航空学报,2025,46(1):1-31,31.

基金项目

国家自然科学基金(12072377) (12072377)

湖南省自然科学基金(2022JJ30678) (2022JJ30678)

航天进入减速与着陆技术实验室开放基金(EDL19092309) National Natural Science Foundation of China(12072377) (EDL19092309)

Natural Science Foundation of Hunan Province(2022JJ30678) (2022JJ30678)

Open Funds of Laboratory of Aerospace Entry,Descent and Landing Technology Foundation(EDL19092309) (EDL19092309)

航空学报

OA北大核心

1000-6893

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