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薄膜增阻球折叠优化设计与展开分析

杨科莹 矫宁 张若楠

航空学报2025,Vol.46Issue(1):129-140,12.
航空学报2025,Vol.46Issue(1):129-140,12.DOI:10.7527/S1000-6893.2024.30849

薄膜增阻球折叠优化设计与展开分析

Folding optimization design and deployment analysis for film drag balloon

杨科莹 1矫宁 1张若楠1

作者信息

  • 1. 北京理工大学 宇航学院,北京 100081
  • 折叠

摘要

Abstract

The drag balloon is one of the primary devices for deorbiting of low Earth orbit spacecraft at the end of their life.Since the thin membrane sphere must be stored in a confined space for an extended period before use,achieving high-density and low-damage folding and smooth inflation and deployment is crucial for its operation.Considering the drag balloon is mostly composed of a certain number of bonded valves,an optimal valve configuration design method that considers shape stability and cost efficiency is firstly proposed.Furthermore,for the single petal structure,a sym-metrical parallel z-type folding scheme is proposed,and methods for quantifying the folded volume and damage are provided.Then,to increase the folding-deployment ratio and reduce crease damage,an optimized folding scheme for the drag balloon is presented,and simulation of a sphere of 6-meter diameter is conducted.Based on this scheme,the effects of valve configuration,inflation speed,and initial internal pressure and temperature on the smooth deploy-ment of the drag balloon are analyzed.The results show that the proposed folding scheme can achieve high-density and low-damage folding of the drag balloon.Additionally,by increasing the number of valves,slowing down the infla-tion speed,avoiding excessive vacuum,and reducing direct sunlight exposure,the attitude oscillation during the de-ployment process can be effectively mitigated,speeding up the attainment of a stable state.

关键词

增阻球/高密度折叠/折痕损伤/折叠方案优化/充气展开

Key words

drag balloon/high-density folding/folding damage/folding scheme optimization/inflatable deployment

分类

航空航天

引用本文复制引用

杨科莹,矫宁,张若楠..薄膜增阻球折叠优化设计与展开分析[J].航空学报,2025,46(1):129-140,12.

基金项目

国家级项目(KJSP2020010301) (KJSP2020010301)

国家自然科学基金(12232003,12102038) National Level Project(KJSP2020010301) (12232003,12102038)

National Natural Science Foundation of China(12232003,12102038) (12232003,12102038)

航空学报

OA北大核心

1000-6893

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