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充气式与机械展开式气动减速器技术研究进展

云成虎 刘党辉 王建华 于沫尧

中国空间科学技术(中英文)2024,Vol.44Issue(6):88-97,10.
中国空间科学技术(中英文)2024,Vol.44Issue(6):88-97,10.DOI:10.16708/j.cnki.1000-758X.2024.0094

充气式与机械展开式气动减速器技术研究进展

Research progress on inflatable and mechanically deployable aerodynamic decelerator technology

云成虎 1刘党辉 1王建华 1于沫尧1

作者信息

  • 1. 航天工程大学宇航科学与技术系,北京 101416
  • 折叠

摘要

Abstract

With the rapid development of the space industry,traditional Entry,Descent,and Landing technologies are failing to meet the demands of modern space missions.Inflatable and mechanically deployable aerodynamic decelerators are expected to be used for the recovery of various space missions due to their foldability,small size and light weight.The research progress and current status are presented around inflatable and mechanically deployable aerodynamic decelerators.Firstly,the flight tests conducted by various countries are introduced on inflatable and mechanically deployable aerodynamic decelerators.Then,it presents the research progress of inflatable aerodynamic decelerator technologies.Four main areas are presented,including structural configuration,aerodynamics,aerothermodynamics and aeroelasticity.Thirdly,the technologies for mechanically deployable aerodynamic decelerators are presented,focusing on the areas of structural design and optimization,aerodynamics,aerothermodynamics,and attitude control.Finally,an insightful perspective on the future technological development of aerodynamic decelerator is presented,highlighting a potential innovative approach for the recovery of launch vehicle sub-stages,spacecraft,and so on.

关键词

充气展开/机械展开/气动减速/EDL技术/柔性/气动特性

Key words

inflatable deployment/mechanical deployment/aerodynamic deceleration/EDL technology/flexibility/aerodynamic characteristics

分类

航空航天

引用本文复制引用

云成虎,刘党辉,王建华,于沫尧..充气式与机械展开式气动减速器技术研究进展[J].中国空间科学技术(中英文),2024,44(6):88-97,10.

基金项目

国家自然科学基金(12003078) (12003078)

中国空间科学技术(中英文)

OA北大核心CSTPCD

1000-758X

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