Author:
Deriglazov A. P.,Tikhonov A. A.
Reference27 articles.
1. V. V. Beletsky and E. M. Levin, Dynamics of Space Tether Systems (Nauka, Moscow, 1990; American Astronautical Society, San Diego, CA, 1993).
2. A. V. Rodnikov and P. S. Krasilnikov, “On spacial motions of an orbital tethered system,” Nelineinaya Din. 13, 505–518 (2017). https://doi.org/10.20537/nd1704004
3. R. L. Forward, Electrodynamic Drag Terminator Tether, Appendix K of High Strength-to-Weight Tapered Hoytether for LEO to GEO Payload Transport, Final Report on NASA SBIR Phase I Contract NAS8-40690 (NASA, 1996).
4. R. L. Forward, R. P. Hoyt, and C. Uphoff, “Application of the Terminator TetherTM electrodynamic drag technology to the deorbit of constellation spacecraft,” in Proc. 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conf. and Exhibit, Cleveland, OH, USA, July 13–15,1998 (American Institute of Aeronautics and Astronautics, New York, 1998), paper No. 98-3491. https://doi.org/10.2514/6.1998-3491.
5. R. L. Forward and R. P. Hoyt, “Terminator TetherTM: A spacecraft deorbit device,” J. Spacecr. Rockets 37, 187–196 (2000). https://doi.org/10.2514/2.3565
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