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Mass Ratio of Electrodynamic Tether to Spacecraft on Deorbit Stability and Efficiency.

Authors :
Changqing Wang
Gangqiang Li
Zhu, Zheng H.
Aijun Li
Source :
Journal of Guidance, Control & Dynamics; Sep2016, Vol. 39 Issue 9, p2187-2194, 8p
Publication Year :
2016

Abstract

The article presents a study related to mass ratio of electrodynamics tether to spacecraft on deorbit stability and efficiency. Topics discussed include ways in which space activities in low Earth orbit have produced a large population of dead bodies, or debris; guidelines to remove or mitigate the space debris; and parametrical analysis of deorbit performance.

Details

Language :
English
ISSN :
07315090
Volume :
39
Issue :
9
Database :
Supplemental Index
Journal :
Journal of Guidance, Control & Dynamics
Publication Type :
Academic Journal
Accession number :
118434063
Full Text :
https://doi.org/10.2514/1.G000429