Magneto-elastic Buckling Analysis of Electrodynamic Space Tethers
Author:
Publisher
National Space Science Center, Chinese Academy of Sciences
Subject
General Medicine
Reference14 articles.
1. ZHONG R, ZHU Z H. Dynamics of nanosatellite deorbit by bare electrodynamic tether in low Earth orbit[J]. J. Spacecraft Rockets, 2013, 50 (3):691-700
2. BOMBARDELLI C, ZANUTTO D, LORENZINI E. Deorbiting performance of bare electrodynamic tethers in inclined orbits[J]. J. Guid. Control Dynam., 2013, 36(5):1550-1556
3. KENTARO L, SATOMI K, YOSHIKI M. Experiments and numerical simulations of an electrodynamic tether deployment from a spool-type reel using thrusters[J]. Acta Astron., 2014, 94(1):318-327
4. STAROSTIN E L, VAN DER HEIJDEN G H M. Theory of equilibria of elastic 2-braids with interstrand interaction[J]. J. Mech. Phys. Solids, 2014, 64:83-132
5. MOON F C. Magnetoelastic instabilities in superconduc-ting structures and Earnshaw's theorem[J]. Mech. Supercond. Struct., 1980, 41:77-90
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