Theoretical and Experimental Investigation of Geomagnetic Energy Effect for LEO Debris Deorbiting
文献类型:期刊论文
作者 | Feng GH(冯冠华); Zhang C(张晨); Zhang H(张珩); Li WH(李文皓); Zhang H(张珩); Li WH(李文皓); Feng GH(冯冠华) |
刊名 | AEROSPACE ; 9 |
出版日期 | 2022-09 |
卷号 | 9页码:511 |
关键词 | LEO debris deorbiting geomagnetic energy (GME) propellant ground proof-of-principle experiment LEO GME utilization |
DOI | 10.3390/aerospace9090511 |
英文摘要 | Space debris is increasingly problematic and needs active removal, especially in low Earth orbits (LEO). Paying for the vast cost of the disposal of debris from the situation is still inevitable even though pivotal technical hurdles have been overcome with the growing maturity of capturing and deorbiting methods. To this end, a 11el geomagnetic energy (GME) propellant approach is firstly proposed to propel a spinning tethered spacecraft for LEO debris deorbiting, without the use of expendable fuel and a large-length tether. In this method, the time-cumulative effect of the interacted torque of the spacecraft's electromagnet and geomagnetic field is used to accelerate the rotating system for GME storage, and the space momentum exchange from the angular momentum of system to the linear momentum of debris is introduced to deorbit the debris for GME release. Next, an on-orbit directional GME storage mechanism is built, and the corresponding two optimal strategies are put forward. Both theoretical and simulation results demonstrate that GME can be stored in the expected direction on any inclined LEO below 1000 km. Deorbiting kg-level debris can be accomplished within several orbital periods with the existing magnetorquer technology. Finally, proof-of-principle experiments of the GME effect are performed and elementarily validate the LEO GME utilization in space. |
学科主题 | Engineering, Aerospace |
分类号 | 二类 |
语种 | 英语 |
WOS记录号 | WOS:000859564500001 |
资助机构 | Strategic Priority Research Program of the Chinese Academy of Sciences [XDA17030200] ; Joint Fund of the Chinese Academy of Sciences [8091A01] ; National Natural Science Foundation of China [11002143] ; [1816318TS00100501] ; [18JSLL0100000505] |
其他责任者 | Li, WH (corresponding author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China. ; Li, WH (corresponding author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China. |
源URL | [http://dspace.imech.ac.cn/handle/311007/90145] |
专题 | 宽域飞行工程科学与应用中心 |
作者单位 | 1.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China 2.Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China |
推荐引用方式 GB/T 7714 | Feng GH,Zhang C,Zhang H,et al. Theoretical and Experimental Investigation of Geomagnetic Energy Effect for LEO Debris Deorbiting[J]. AEROSPACE, 9,2022,9:511. |
APA | 冯冠华.,张晨.,张珩.,李文皓.,Zhang H.,...&Feng GH.(2022).Theoretical and Experimental Investigation of Geomagnetic Energy Effect for LEO Debris Deorbiting.AEROSPACE,9,511. |
MLA | 冯冠华,et al."Theoretical and Experimental Investigation of Geomagnetic Energy Effect for LEO Debris Deorbiting".AEROSPACE 9(2022):511. |
入库方式: OAI收割
来源:力学研究所
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