Optimal design and current control strategies of an electrodynamic tape for ISS station-keeping-Reference-Cited by-同舟云学术

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Optimal design and current control strategies of an electrodynamic tape for ISS station-keeping

Published:2024-10 Issue: Volume:223 Page:621-629
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Brunello A.^ORCID,Anese G.^ORCID,Borderes-Motta G.^ORCID,Valmorbida A.^ORCID,Sánchez-Arriaga G.^ORCID,Lorenzini E.C.^ORCID

Publisher

Elsevier BV

Reference34 articles.

1. Theoretical model of drag force impact on a model international space station satellite due to solar activity;Nwankwo;Trans. Japan Soc. Aeronaut. Space Sci., Aerosp. Technol. Japan,2014

2. Impact risk assessment of deorbiting strategies in low earth orbits;Sarego,2021

3. Bare tethers for electrodynamic spacecraft propulsion;Estes;J. Spacecr. Rockets,2000

4. Concept of combined electrorocket and electrodynamic propulsion system for stati on keeping of large space structures;Strashinsky,2004

5. Space station reboost with electrodynamic tethers;Vas;J. Spacecr. Rockets,2000

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