| Development of a novel wave plasma propulsion module with six-directional thrust vectoring capability AI Shumeiko, VD Telekh, VI Mayorova Acta Astronautica 191, 431-437, 2022 | 18 | 2022 |
| Helicon engine in outboard air as a successful solution for maintaining small space vehicle in orbits up to 200 km AI Shumeiko, VD Telekh AIP Conference Proceedings 2171 (1), 2019 | 15 | 2019 |
| Probe diagnostics and optical emission spectroscopy of wave plasma source exhaust AI Shumeiko, VD Telekh, SV Ryzhkov Symmetry 14 (10), 1983, 2022 | 13 | 2022 |
| Probe diagnostics of the plasma plume created by a magnetic nozzle of an inductively coupled plasma source AI Shumeiko, VD Telekh Journal of Physics: Conference Series 1393 (1), 012027, 2019 | 11 | 2019 |
| Development of a six-directional plasma propulsion module for small satellites A Shumeiko, V Telekh, V Mayorova Proceedings of the International Astronautical Congress, IAC, 2020 | 6 | 2020 |
| Advanced wave plasma thruster with multiple thrust vectoring capability AI Shumeiko, FS Jarrar, SS Swei AIAA SCITECH 2022 Forum, 2190, 2022 | 4 | 2022 |
| Development of novel electrodeless plasma thruster with multiple thrust vectoring capability AI Shumeiko, F Jarrar, SSM Swei Proceedings of the International Astronautical Congress, IAC 4, 2021 | 4 | 2021 |
| Nature-inspired concepts for high-power electric propulsion systems AI Shumeiko Fusion Science and Technology 80 (7), 856-869, 2024 | 3 | 2024 |
| Starting Modes of Bi-Directional Plasma Thruster Utilizing Krypton AI Shumeiko, VD Telekh, SV Ryzhkov Symmetry 15 (9), 1705, 2023 | 3 | 2023 |
| Direct thrust measurements of 2U-sized bi-directional wave plasma thruster AI Shumeiko, VD Telekh AIP Advances 13 (8), 2023 | 3 | 2023 |
| Determination of the minimum size of a small spacecraft of the cubesat standard for the possibility of using modern propulsion systems AD Pashaev, AI Shumeiko, VD Telekh AIP Conference Proceedings 2549 (1), 2023 | 3 | 2023 |
| Определение минимального размера малого космического аппарата стандарта Cubesat для возможности использования современных двигательных установок АИ Шумейко, АД Пашаев, ВД Телех XLV Академические чтения по космонавтике, посвященные памяти академика СП …, 2021 | 2 | 2021 |
| Numerical simulation of thermo-throttle for iodine flow rate control in multidirectional plasma thruster P Savelev, A Pashaev, A Shumeiko Nuclear Science and Technology Open Research 1 (12), 12, 2023 | 1 | 2023 |
| Data sheet of iodine vapor flow rates v1 A Shumeiko OSF, 2023 | 1 | 2023 |
| Modeling of processes in porous thermal throttles for iodine flow control for space applications PO Savelev, AD Pashaev, AI Shumeiko Results in Engineering 24, 103463, 2024 | | 2024 |
| Electrodeless plasma thruster with closed-ring-shaped gas discharge chamber AI Shumeiko, FS Jarrar, SSM Swei US Patent 12,012,234, 2024 | | 2024 |
| Bi-Directional Wave Plasma Thruster characteristics A Shumeiko OSF, 2024 | | 2024 |
| Probe diagnostics and optical emission spectroscopy of the plasma plume created by a magnetic nozzle of an inductively coupled plasma source AR Gizzatullin, AI Shumeiko, VD Telekh Энергетика, инфокоммуникационные технологии и высшее образование, 175-180, 2023 | | 2023 |
| Bi-directional wave plasma thruster for spacecraft AI Shumeiko US Patent App. 17/343,993, 2022 | | 2022 |
| Development of a Bi-Directional Wave Plasma Thruster for Small Satellites A Shumeiko | | 2022 |
Sergei RyzhkovBauman Moscow State Technical University在 bmstu.ru 的电子邮件经过验证
Sergei RyzhkovBauman Moscow State Technical University在 bmstu.ru 的电子邮件经过验证