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A Comparison of Characteristics of a Model of the Anode Layer Thruster Operating on Xenon, Argon and Nitrogen
| Authors: Dukhopelnikov D.V., Ryаzanov V.A., Shilov S.O. | Published: 26.07.2018 |
| Published in issue: #7(700)/2018 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: electric rocket propulsion unit, anode layer thruster, reactive gas, ambient air, ion current, power thrust ratio |
