The analysis of operability of dilatometric microthruster with polymer working components

The article describes the device of a dilatometric microthruster. The study of the device's operability with low power consumption is carried out. It is based on the designed prototype of the thruster in vacuum conditions. The results of the experiments showed that at the pressure of the work...

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Main Authors: M. V. Smagin, E. E. Kolyagin, I. S. Vavilov
Format: Article
Language:English
Published: Omsk State Technical University, Federal State Budgetary Educational Institution of Higher Education 2023-12-01
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/2023/%D0%A2.7,%20%E2%84%964%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/72-78%20%D0%A1%D0%BC%D0%B0%D0%B3%D0%B8%D0%BD%20%D0%9C.%20%D0%92.,%20%D0%9A%D0%BE%D0%BB%D1%8F%D0%B3%D0%B8%D0%BD%20%D0%95.%20%D0%95.,%20%D0%92%D0%B0%D0%B2%D0%B8%D0%BB%D0%BE%D0%B2%20%D0%98.%20%D0%A1..pdf
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author M. V. Smagin
E. E. Kolyagin
I. S. Vavilov
author_facet M. V. Smagin
E. E. Kolyagin
I. S. Vavilov
author_sort M. V. Smagin
collection DOAJ
description The article describes the device of a dilatometric microthruster. The study of the device's operability with low power consumption is carried out. It is based on the designed prototype of the thruster in vacuum conditions. The results of the experiments showed that at the pressure of the working gas-air mixture at the thruster inlet of 1 atm. and with a mass flow rate of gas 2,33•10–7 kg/s, the device is able to produce a thrust value within 33 mkH, with a specific thrust pulse of 140 m/s. In turn, the power consumption of the device is only 0,81 W.
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series Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
spelling doaj.art-a6d3d60e48984b249cea8c314ca8b8902023-12-25T10:29:45ZengOmsk State Technical University, Federal State Budgetary Educational Institution of Higher EducationОмский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"2588-03732587-764X2023-12-0174727810.25206/2588-0373-2023-7-4-72-78The analysis of operability of dilatometric microthruster with polymer working componentsM. V. Smagin0https://orcid.org/0000-0002-6878-1742E. E. Kolyagin1https://orcid.org/0009-0001-7059-9165I. S. Vavilov2Omsk State Technical UniversityOmsk State Technical UniversityOmsk State Technical UniversityThe article describes the device of a dilatometric microthruster. The study of the device's operability with low power consumption is carried out. It is based on the designed prototype of the thruster in vacuum conditions. The results of the experiments showed that at the pressure of the working gas-air mixture at the thruster inlet of 1 atm. and with a mass flow rate of gas 2,33•10–7 kg/s, the device is able to produce a thrust value within 33 mkH, with a specific thrust pulse of 140 m/s. In turn, the power consumption of the device is only 0,81 W.https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2023/%D0%A2.7,%20%E2%84%964%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/72-78%20%D0%A1%D0%BC%D0%B0%D0%B3%D0%B8%D0%BD%20%D0%9C.%20%D0%92.,%20%D0%9A%D0%BE%D0%BB%D1%8F%D0%B3%D0%B8%D0%BD%20%D0%95.%20%D0%95.,%20%D0%92%D0%B0%D0%B2%D0%B8%D0%BB%D0%BE%D0%B2%20%D0%98.%20%D0%A1..pdfmicrothrusterdilatometric microthrustercold gasenergy efficiencythrustspecific thrust impulse
spellingShingle M. V. Smagin
E. E. Kolyagin
I. S. Vavilov
The analysis of operability of dilatometric microthruster with polymer working components
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
microthruster
dilatometric microthruster
cold gas
energy efficiency
thrust
specific thrust impulse
title The analysis of operability of dilatometric microthruster with polymer working components
title_full The analysis of operability of dilatometric microthruster with polymer working components
title_fullStr The analysis of operability of dilatometric microthruster with polymer working components
title_full_unstemmed The analysis of operability of dilatometric microthruster with polymer working components
title_short The analysis of operability of dilatometric microthruster with polymer working components
title_sort analysis of operability of dilatometric microthruster with polymer working components
topic microthruster
dilatometric microthruster
cold gas
energy efficiency
thrust
specific thrust impulse
url https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2023/%D0%A2.7,%20%E2%84%964%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/72-78%20%D0%A1%D0%BC%D0%B0%D0%B3%D0%B8%D0%BD%20%D0%9C.%20%D0%92.,%20%D0%9A%D0%BE%D0%BB%D1%8F%D0%B3%D0%B8%D0%BD%20%D0%95.%20%D0%95.,%20%D0%92%D0%B0%D0%B2%D0%B8%D0%BB%D0%BE%D0%B2%20%D0%98.%20%D0%A1..pdf
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