Dilatometric Microdrive of small spacecraft with resonant microwave accelerator
The article contains the research of the authors in the field of jet propulsion systems with low energy consumption of small spacecraft (SSC) of nanosatellite class. The paper presents the concept of a Microdrive combining thermogasdynamic and electrodynamic methods of creating a jet thrust. We a...
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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
2018-12-01
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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/2018/%D0%A2.%202,%20%E2%84%96%204/36-41%20%D0%92%D0%B0%D0%B2%D0%B8%D0%BB%D0%BE%D0%B2%20%D0%98.%20%D0%A1.,%20%D0%9B%D1%83%D0%BA%D1%8C%D1%8F%D0%BD%D1%87%D0%B8%D0%BA%20%D0%90.%20%D0%98.,%20%D0%AF%D1%87%D0%BC%D0%B5%D0%BD%D0%B5%D0%B2%20%D0%9F.%20%D0%A1.%20%D0%B8%20%D0%B4%D1%80..pdf |
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| Summary: | The article contains the research of the authors in the field of jet propulsion systems with low energy
consumption of small spacecraft (SSC) of nanosatellite class. The paper presents the concept of
a Microdrive combining thermogasdynamic and electrodynamic methods of creating a jet thrust. We
are talking about the propulsion system with resonance accelerating system, pre-heated and ionized
working fluid. A toroidal volume resonator excited by a low-power solid-state microwave oscillator is
considered as an accelerator.
The work has experimental and theoretical components. The experimental part is devoted to the
development of a method for transmitting microwave energy to a volume resonator from an oscillator.
The theoretical part includes the calculation of the accelerating gap, the dimensions of the toroidal
resonator, the estimation of the working fluid velocity after preheating and acceleration.
This work is a continuation of works on creation of methodological bases for design correction engine
micro thrust µa with microwave acceleration of the working body |
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| ISSN: | 2588-0373 2587-764X |