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: I. S. Vavilov, A. I. Lykyanchik, P. S. Yachmenev, R. N. Litau, I. A. Kuzmenko
Format: Article
Language:English
Published: Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education 2018-12-01
Series:Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
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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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author I. S. Vavilov
A. I. Lykyanchik
P. S. Yachmenev
R. N. Litau
I. A. Kuzmenko
author_facet I. S. Vavilov
A. I. Lykyanchik
P. S. Yachmenev
R. N. Litau
I. A. Kuzmenko
author_sort I. S. Vavilov
collection DOAJ
description 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
format Article
id doaj-art-d1ba30a1d8234dbea12f41262a7aa63c
institution Kabale University
issn 2588-0373
2587-764X
language English
publishDate 2018-12-01
publisher Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education
record_format Article
series Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
spelling doaj-art-d1ba30a1d8234dbea12f41262a7aa63c2025-02-02T19:19:28ZengOmsk State Technical University, Federal State Autonomous Educational Institution of Higher EducationОмский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"2588-03732587-764X2018-12-0124364110.25206/2588-0373-2018-2-4-36-41Dilatometric Microdrive of small spacecraft with resonant microwave acceleratorI. S. Vavilov0A. I. Lykyanchik1https://orcid.org/0000-0002-3309-4125P. S. Yachmenev2https://orcid.org/0000-0003-3483-4321 R. N. Litau3I. A. Kuzmenko4Omsk State Technical UniversityOmsk State Technical UniversityOmsk State Technical UniversityOmsk State Technical UniversityOmsk State Technical UniversityThe 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 bodyhttps://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..pdfsmall spacecraftnitrogentractiona resonant cavitymicrowaveplasmathe gas passage
spellingShingle I. S. Vavilov
A. I. Lykyanchik
P. S. Yachmenev
R. N. Litau
I. A. Kuzmenko
Dilatometric Microdrive of small spacecraft with resonant microwave accelerator
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
small spacecraft
nitrogen
traction
a resonant cavity
microwave
plasma
the gas passage
title Dilatometric Microdrive of small spacecraft with resonant microwave accelerator
title_full Dilatometric Microdrive of small spacecraft with resonant microwave accelerator
title_fullStr Dilatometric Microdrive of small spacecraft with resonant microwave accelerator
title_full_unstemmed Dilatometric Microdrive of small spacecraft with resonant microwave accelerator
title_short Dilatometric Microdrive of small spacecraft with resonant microwave accelerator
title_sort dilatometric microdrive of small spacecraft with resonant microwave accelerator
topic small spacecraft
nitrogen
traction
a resonant cavity
microwave
plasma
the gas passage
url 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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AT psyachmenev dilatometricmicrodriveofsmallspacecraftwithresonantmicrowaveaccelerator
AT rnlitau dilatometricmicrodriveofsmallspacecraftwithresonantmicrowaveaccelerator
AT iakuzmenko dilatometricmicrodriveofsmallspacecraftwithresonantmicrowaveaccelerator