Abstract
Two important applications of electrodynamics tethers, among others, are those of using them for deorbiting and/or propulsion. A crucial issue for both of the above applications is the dynamic stability of the tether system. The electrodynamic forces on the tether couple, in fact, in-plane and out-of-plane oscillations and, especially for light systems, can drive the tethers unstable. In both the applications of deorbiting and propulsion, the tether system is supposed to operate for long intervals of time (months) so that a crucial issue, in view of the fact that the system is potentially unstable, is that of analyzing the constraints to ensure long term safe operations (i.e. with the tether oscillation amplitudes below certain limits). In this paper we consider this issue referring for the lateral oscillations of a flexible tether. We refer to a bare conducting tether with the current to the various tether elements calculated from plasma theory. In addition, we impose a time variation of the current and model the response to changes in ionospheric density.
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Dobrowolny, M. Lateral Oscillations of an Electrodynamic Tether. J of Astronaut Sci 50, 125–147 (2002). https://doi.org/10.1007/BF03546259
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DOI: https://doi.org/10.1007/BF03546259