Analysis of Bare-Tether Systems for Deorbiting Low-Earth-Orbit Satellites
Author:
Affiliation:
1. Universidad Politecnica de Madrid, 28040 Madrid, Spain
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3820
Reference21 articles.
1. Bare wire anodes for electrodynamic tethers
2. Propulsive Small Expendable Deployer System Experiment
3. Terminator Tether: A Spacecraft Deorbit Device
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