Calorimetric studies of microwave ion thruster

The authors continue their work in the field of calorimetric studies of the parameters of an accelerated ionized gas jet of prototypes of microwave ion micro-thrusters with an energy consumption of up to 10 watts. This paper presents an improved calorimetric method. The introduction into the desig...

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Main Authors: I. S. Vavilov, K. I. Zharikov, P. S. Yachmenev, V. V. Fedyanin, P. V. Stepen, A. I. Lukyanchuk, I. A. Kuzmenko
Formato: Artigo
Idioma:Inglês
Publicado em: Omsk State Technical University, Federal State Budgetary Educational Institution of Higher Education 2022-03-01
Colecção:Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
Assuntos:
calorimeter
microwave
plasma
small spacecraft
nitrogen
thrust
speed
thermal imager
Acesso em linha: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)/118-127%20%D0%92%D0%B0%D0%B2%D0%B8%D0%BB%D0%BE%D0%B2%20%D0%98.%20%D0%A1.,%20%D0%96%D0%B0%D1%80%D0%B8%D0%BA%D0%BE%D0%B2%20%D0%9A.%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%A4%D0%B5%D0%B4%D1%8F%D0%BD%D0%B8%D0%BD%20%D0%92.%D0%92.%20%D0%B8%20%D0%B4%D1%80.pdf
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