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