Two-gaps microwave ion engine and its study by aerodynamic method
The article contains the authors’ research in the field of jet propulsion systems with low energy consumption of small spacecraft of the class of nanosatellites. The paper presents a microwave ion engine with double acceleration of ionized gas in the gaps formed by the end surfaces of cylindrical...
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Main Authors: | , , , , , , |
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Format: | Article |
Language: | English |
Published: |
Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education
2022-03-01
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Series: | Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" |
Subjects: | |
Online Access: | https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2022/%D0%A2.%206,%20%E2%84%961%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/109-117%20%D0%92%D0%B0%D0%B2%D0%B8%D0%BB%D0%BE%D0%B2%20%D0%98.%20%D0%A1.,%20%D0%AF%D1%87%D0%BC%D0%B5%D0%BD%D0%B5%D0%B2%20%D0%9F.%20%D0%A1.,%20%D0%A4%D0%B5%D0%B4%D1%8F%D0%BD%D0%B8%D0%BD%20%D0%92.%20%D0%92.,%20%D0%96%D0%B0%D1%80%D0%B8%D0%BA%D0%BE%D0%B2%20%D0%9A.%20%D0%98.%20%D0%B8%20%D0%B4%D1%80.pdf |
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Summary: | The article contains the authors’ research in the field of jet propulsion systems with low energy
consumption of small spacecraft of the class of nanosatellites. The paper presents a microwave ion
engine with double acceleration of ionized gas in the gaps formed by the end surfaces of cylindrical
resonators. The results of an experimental study of the pressure force of a jet set of ionized gas by the
aerodynamic double angle method are presented. A stand for determining the power parameters of
week plasmajet is presented. The design of the prototype is presented. The total energy consumption
of the prototype is 5 watts, the accelerated gas flow rate is up to 200 km/s, the jet pressure force on
the sensing element of the stand is 0,1 μN. The working body of the prototype is nitrogen at a pressure
in a vacuum chamber of 18 Pa. |
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ISSN: | 2588-0373 2587-764X |