The status of space debris and the development of small satellite constellation are introduced at first.The advantages of the space debris removal membrane sail are proposed,such as low cost,high degree of technological maturity and good applicability for all kinds of LEO satellites.The studies on membrane sail for space debris removal are summarized,as well as the latest flight tests.Key technologies associated with the de-orbit sail are presented,such as modeling and simulation technology for de-orbit efficiency,collision risk analysis and protection design,folding and deploying technology and long life membrane technology,and the approaches to solve these key problems are given.The flight test of TAURUS satellite with membrane sail is presented,and the comparison of de-orbit flight efficiency with the simulation results are given,the 50% of membrane sail area is proposed to be used as the average de-orbit sail area for satellite whose attitude is out of control,and the follow-up development of the TAURUS membrane sail is introduced.
YUN Wei-dong
,
FANG Guang-qiang
,
FU Yu-lei
,
DAI Hua-jie
,
ZHENG Qi
,
WANG Zhi-yi
,
SHI Fei-zhou
. The Progress and Applications of Deployable Membrane Sail for Space Debris Removal[J]. Journal of Space Science and Experiment, 2021
, 21(3)
: 20
-28
.
DOI: 10.19963/j.cnki.2096-4099.2021.03.003
[1] Liou J C.USA space debris environment,operations,and research updates.In:54th Session of the Scientific and Technical Subcommittee,Committee on the Peaceful Uses of Outer Space.Vienna:UNCOPOUS,2017.
[2] 李明,龚自正,刘国青.空间碎片监测移除前沿技术与系统发展[J].科学通报,2018,63(25):2570—2591.
[3] 陆震.小卫星和微纳卫星应用现状与挑战[J].兵器装备工程学报,2018,6:1—7.
[4] 何慧东,付郁.2017年全球小卫星发展回顾[J].国际太空,2018.2:51—56.
[5] Biddy C,Svitek T.LightSail-1 solar sail design and qualification[C] //Jet Propulsion Lab.Proceedings of the 41st Aerospace Mechanisms Symposium,May 16-18,2012,Pasadena,Ca.Pasadena:JPL,2012:1319.
[6] Hillebrandt M,Meyer S,Zander M.Deployment testing of the de-orbit sail flight hardware[C] //American Institute of Aeronautics and Astronautics.2nd AIAA Spacecraft Structures Conference,January 5-9 2015,Kissimmee,Florida.Washington:AIAA,2015:0434.
[7] Ryszawa E,Roszkowski D.PW-Sat2 preliminary design review[R].Warsaw University of Technology.Warsaw:WUT.2016.
[8] 曾玉堂.立方体卫星制动帆离轨装置的设计与研究[D].南京:南京理工大学,2017.
[9] 陈险峰,任维佳,李晓明.小卫星主动离轨技术的设计与实践[C].第十届全国空间碎片学术会议论文集.2019.11.
[10] Fitié A,Breukelen E,Rotteveel J.Inflatable aerobrake for end-of-life de-orbit of nanosatellites performance evaluation and collision risk assessment[C] //International Astronautical Federation.59th International Astronautical Congress,September 29,2008-October 3,2008,Glasgow,United kingdom.Paris:IAF,2008:2398—3406.
[11] Lourens Visagie,Vaios Lappas,Sven Erb..Drag sails for space debris mitigation.Acta Astronautica[J].2015,109:65—75.
[12] Arya M,Pellegrino S.Deployment mechanics of highly compacted thin membrane structure[C] //American Institute of Aeronautics and Astronautics.Spacecraft Structures Conference,January 13-17 2014,National Harbor,Maryland.Washington:AIAA,2014: 1038.
[13] Shirasawa Y,Mori O,Sawada H.A study on membrane dynamics and deformation of solar power sail demenstrator IKAROS[C] //American Institute of Aeronautics and Astronautics.53rd AIAA/ASME/AS CE/AHS/ASC Structures,Structural Dynamics and Materials Conference,April 23-26 2012,Ho-nolulu,Hawaii.Washington:AIAA,2012:1747.
[14] Tsuda Y,Mori O,Funase R,Achievement of IKA-ROS-Japanese deep space solar sail demonstration mission[J].Acta Astronautica,2013,82:183—188.
[15] Sawada H,Shirasawa Y,Mori O.On-orbit result and analysis of sail deployment of world's first solar power sail IKAROS[J].Japanese Rocket Society,2012,27(1):54—68.
[16] Shirasawa Y,Mori O,Miyazaki Y.Analysis of Membrane Dynamics using Multi-Particle Model for solar sail demonstrator IKAROS[C] //American Institute of Aeronautics and Astronautics.52nd AIAA/ASM E/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference,April 4-7 2011,Denver,Colorado.Washington:AIAA,2011:1890.
[17] Torisaka A,Satoh Y,Akita T.Membrane space structure with sterical support of booms and cables[C] //American Institute of Aeronautics and Astronautics.3rd AIAA Spacecraft Structures Conference,January 4-8 2016,San Diego,California,USA.Washington:AIA A,2016:1217.
[18] Arya M,Lee N,Pellegrino S.Wrapping thick membranes with slipping folds[C] //American Institute of Aeronautics and Astronautics.2nd AIAA Spacecraft Structures Conference,January 5-9 2015,Kissimmee,Florida.Washington:AIAA,2015:0682.
[19] Bousquet P,Dupuy C,Bonnefond T.De-orbiting Microscope spacecraft by drag enhancement[C] //International Academy of Astronautics.57th International Astronautical Congress,October 2-6 2006,Valencia,Spain.Paris:IAA,2006:6405.
[20] Thomas G M.Prototype development and dynamic characterization of deployable cubesat booms[C] //American Institute of Aeronautics and Astronautics.51st AIA A/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference,April 12 2010-April 15 2010,Orlando,FL,United States,Washington:AIAA,2010:2907.
[21] Roybal F A,Banik J A,Murphey T W.Development of an elastically deployable boom for tensioned planar structures[C] //American Institute of Aeronautics and Astronautics.48th AIAA/ASME/ASCE/AHS/AS C Structures,Structural Dynamics,and Materials Conference,April 23-26 2007,Honolulu,Hawaii.Washington:AIAA,2007:1838.
[22] Sobey A R.Design and Development of NEA scout solar sail deployer mechanism[C] //National Aeronautics and Space Administration,43rd Aerospace Mechanisms Symposium,May 4-6,2016,Ames Research Center.Huntsville:NASA,2016:14.
[23] 沈自才,张帆,赵春晴.IKAROS太阳帆的关键技术分析与启示[J].航天器工程,2012.4,101—107.
[24] Shen Zicai,Zhang Fan,Zhao Chunqing.Key technology analysis and enlightenment of IKAROS solar sail[J].Spacecraft Engineering.2012.4,101—107.
[25] 陈罗婧,王沫,吕秋杰.国外太阳帆薄膜材料选择及帆面展开方式研究进展[J].空间电子技术,2015,3,:18—26.
[26] 傅宇蕾.离轨薄膜帆原子氧侵蚀的缺陷密度效应数值模拟研究[J].空间碎片研究,2020,20(2):14—21.
