Stability and control of electrodynamic tethers for de-orbiting applications-Reference-Cited by-同舟云学术

Stability and control of electrodynamic tethers for de-orbiting applications

Published:2001-03 Issue:5-12 Volume:48 Page:491-501
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Corsi J.,Iess L.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference10 articles.

1. Satellite Deorbiting by means of Electrodynamic Tethers: General Concepts and Requirements;Iess;49th International Astronautical Congress, IAF-98-S.6.05,2821998

2. Electrodynamic Tethers for Deorbiting Applications;Vannaroni;50th IAF Meeting, IAA-99-6.6.08,481999

3. Space Electrodynamic Tether Propulsion Technology: System considerations & Future Plans;Gilchrist;35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA 99-2841,20241999

4. Performance of the Terminator Tether™ for Autonomous Deorbit of LEO Spacecraft;Hoyt;35th AIAA-ASME-SAE-ASEE Joint Propulsion Conference and Exhibit, AIAA 99-2841,20241999

5. Bare Wire Anode for Electrodynamic Tethers;Sammartin;Journal of Propulsion and Power,1993

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