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...
| _version_ | 1811329745784143872 |
|---|---|
| author | I. S. Vavilov P. S. Yachmenev V. V. Fedyanin K. I. Zharikov P. V. Stepen A. I. Lukyanchuk I. A. Kuzmenko |
| author_facet | I. S. Vavilov P. S. Yachmenev V. V. Fedyanin K. I. Zharikov P. V. Stepen A. I. Lukyanchuk I. A. Kuzmenko |
| author_sort | I. S. Vavilov |
| collection | DOAJ |
| description | 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. |
| first_indexed | 2024-04-13T15:49:21Z |
| format | Article |
| id | doaj.art-038b32ba09e540debfcdbae5f113592c |
| institution | Directory Open Access Journal |
| issn | 2588-0373 2587-764X |
| language | English |
| last_indexed | 2024-04-13T15:49:21Z |
| publishDate | 2022-03-01 |
| publisher | Omsk State Technical University, Federal State Budgetary Educational Institution of Higher Education |
| record_format | Article |
| series | Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" |
| spelling | doaj.art-038b32ba09e540debfcdbae5f113592c2022-12-22T02:40:52ZengOmsk State Technical University, Federal State Budgetary Educational Institution of Higher EducationОмский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"2588-03732587-764X2022-03-016110911710.25206/2588-0373-2022-6-1-109-117Two-gaps microwave ion engine and its study by aerodynamic methodI. S. Vavilov0P. S. Yachmenev1https://orcid.org/0000-0003-3483-4321V. V. Fedyanin2https://orcid.org/0000-0003-3126-9865K. I. Zharikov3https://orcid.org/0000-0002-4966-1788P. V. Stepen4A. I. Lukyanchuk5https://orcid.org/0000-0002-3309-4125I. A. Kuzmenko6Omsk State Technical UniversityOmsk State Technical UniversityOmsk State Technical UniversityOmsk State Technical UniversityOmsk State Technical UniversityOmsk State Technical UniversityOmsk State Technical UniversityThe 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. 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.pdfvolumetric resonatormicrowaveplasmasmall spacecraftnitrogenthrustspeed |
| spellingShingle | I. S. Vavilov P. S. Yachmenev V. V. Fedyanin K. I. Zharikov P. V. Stepen A. I. Lukyanchuk I. A. Kuzmenko Two-gaps microwave ion engine and its study by aerodynamic method Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" volumetric resonator microwave plasma small spacecraft nitrogen thrust speed |
| title | Two-gaps microwave ion engine and its study by aerodynamic method |
| title_full | Two-gaps microwave ion engine and its study by aerodynamic method |
| title_fullStr | Two-gaps microwave ion engine and its study by aerodynamic method |
| title_full_unstemmed | Two-gaps microwave ion engine and its study by aerodynamic method |
| title_short | Two-gaps microwave ion engine and its study by aerodynamic method |
| title_sort | two gaps microwave ion engine and its study by aerodynamic method |
| topic | volumetric resonator microwave plasma small spacecraft nitrogen thrust speed |
| url | 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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