Research of design of a small spacecraft with an electrothermal propulsion system

Research of design of a small spacecraft with an electrothermal propulsion system

The paper presents the results of solving the multivariate problem of forming the design of a small spacecraft with various propulsion systems based on freons with electrothermal thrusters. As initial data, the required reserves of characteristic velocities for maintaining the active lifetime for...

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Bibliographic Details
Main Author: P. S. Yachmenev
Format: Article
Language:English
Published: Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education 2022-12-01
Series:Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
Subjects:
small spacecraft
low-orbit grouping
propulsion system
electrothermal thruster
random search method
prioritization method
Online Access:https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2022/%D0%A2.6%20%E2%84%964%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/60-68%20%D0%AF%D1%87%D0%BC%D0%B5%D0%BD%D0%B5%D0%B2%20%D0%9F.%20%D0%A1..pdf

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https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2022/%D0%A2.6%20%E2%84%964%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/60-68%20%D0%AF%D1%87%D0%BC%D0%B5%D0%BD%D0%B5%D0%B2%20%D0%9F.%20%D0%A1..pdf

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