A new Ballistic Limit Equation for thin tape tethers
Author:
Funder
European Commission
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference15 articles.
1. P.D. Anz-Meador, Tether-debris interactions in low Earth orbit, in: Proceedings of the AIP Conference, vol. 552, February 2001, pp. 525.
2. C. Pardini, T. Hanada, P.H. Krisko, Benefits and risks of using electrodynamic tethers to de-orbit spacecraft, in: Proceedings of the 57th International Astronautical Congress (IAC2006), Valencia (Spain), Oct. 2–6, 2006.
3. Are de-orbiting missions possible using electrodynamic tethers? Task review from the space debris perspective;Pardini;Acta Astronaut.,2007
4. Benefits and risk of using electrodynamic tethers to de-orbit spacecraft;Pardini;Acta Astronaut.,2009
5. Survival probability of round and tape tethers against debris impact;Khan;J. Spacecr. Rockets,2013
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