空间增阻薄膜结构研究进展及关键技术

doi:10.3901/JME.2020.13.156

机械工程学报 ›› 2020, Vol. 56 ›› Issue (13): 156-164.doi: 10.3901/JME.2020.13.156

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空间增阻薄膜结构研究进展及关键技术

彭福军^1,2, 恽卫东^1,2, 耿海峰^1,2

1. 上海宇航系统工程研究所上海 201108;
2. 上海市空间飞行器机构重点实验室上海 201108

收稿日期:2019-09-01 修回日期:2020-03-13 出版日期:2020-07-05 发布日期:2020-08-01
通讯作者: 彭福军(通信作者),男,1969年出生,博士,研究员。主要研究方向为空间结构与机构技术。E-mail:pfj_tj@126.com
作者简介:恽卫东,男,1985年出生,硕士,高级工程师。主要研究方向为空间结构与机构技术。E-mail:clarence04@163.com
基金资助:
国防科技工业局空间碎片专项资助项目（KJSP2016040203）。

Advancement and Key Technologies of Deployable Membrane Structure for Space Debris Removal

PENG Fujun^1,2, YUN Weidong^1,2, GENG Haifeng^1,2

1. Shanghai Institute of Aerospace System Engineering, Shanghai 201108;
2. Shanghai Key Laboratory of Spacecraft Mechanism, Shanghai 201108

Received:2019-09-01 Revised:2020-03-13 Online:2020-07-05 Published:2020-08-01

摘要/Abstract

摘要： 概述空间碎片的严峻形势和碎片减缓领域未来趋势，梳理国内外小卫星星座计划，介绍卫星离轨规范问题最新进展；提出空间增阻薄膜结构技术因成本低、技术成熟度高，对不同规格低轨道类航天器具有很好适用性，最易于推广应用于空间碎片减缓；对空间增阻薄膜结构技术国内外发展现状进行梳理，并提出空间增阻薄膜结构主要关键技术，对增阻薄膜结构构型设计技术、长寿命材料技术、折叠展开技术和低成本设计技术等进行分析。分析表明，未来星座计划迅速发展将进一步加剧空间碎片严峻形势；现有的碎片减缓规则不能满足要求，新的规则将很快推出，对增阻离轨薄膜结构技术提出了迫切需求；目前空间增阻薄膜结构的主要关键技术都取得了突破，并已完成搭载验证，具备用于卫星离轨的条件。

关键词: 空间碎片, 离轨, 薄膜结构

Abstract: The status of space debris and removal technology were introduced at first. The development of small satellite constellation and study on de-orbit specification of satellite were summarized. The advancement of the space debris removal membrane structure was proposed due to its unique properties such as low cost, high degree of technological maturity and good applicability for all kinds of LEO satellites. Key technologies associated with the membrane structure were presented, such as structure configuration design technology, long life membrane technology, fold and deploy technology, low cost design technology, and the approaches to solve these key problems were introduced. The analysis showed that the status of space debris will be even more threatening due to the rapid development of small satellite constellation, new de-orbit specification of satellite will be promulgated soon, the application of space debris removal membrane structure was urgently demanded. The main technologies associated with the membrane structure had been studied and tested in space flight, the technique will be widely applied in the future.

Key words: space debris, de-orbit removal, membrane structure

中图分类号:

V423

彭福军, 恽卫东, 耿海峰. 空间增阻薄膜结构研究进展及关键技术[J]. 机械工程学报, 2020, 56(13): 156-164.

PENG Fujun, YUN Weidong, GENG Haifeng. Advancement and Key Technologies of Deployable Membrane Structure for Space Debris Removal[J]. Journal of Mechanical Engineering, 2020, 56(13): 156-164.

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空间增阻薄膜结构研究进展及关键技术

Advancement and Key Technologies of Deployable Membrane Structure for Space Debris Removal

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