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Evaluation of relative final mass of a nanosatellite delivered to the near-earth space using a pulsed launcher and a pulsed correcting thruster
| Authors: Gerasimov Yu.V., Karetnikov G.K., Selivanov A.B., Fionov A.S. | Published: 11.09.2013 |
| Published in issue: #3(92)/2013 | |
| DOI: | |
| Category: Contemporary Problems of Mechanical Engineering | |
| Keywords: nanosatellite, space transportation systems, pulsed launch, cluster space systems | |