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Employing a tether system for a Mars mission
| Authors: Birev N.V. | Published: 02.12.2016 |
| Published in issue: #3(3)/2016 | |
| DOI: DOI: 10.18698/2541-8009-2016-3-22 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: tether system, spacecraft, orbit, tethered platform, delta-v, linear velocity, angular velocity, elliptical orbital velocity | |