Studies of the design layout of resistojet with porous structure for propulsion systems of small spacecraft

Studies of the design layout of resistojet with porous structure for propulsion systems of small spacecraft

The results of experimental studies on nitrogen with an overpressure of 0,02 MPa resistojet propulsion system of a small spacecraft with a porous structure weighing 45 g and an autonomous heating element with a radius of 3 mm with a power consumption of up to 60 watts for a warm-up time of up to 3...

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Bibliographic Details
Main Authors: V. N. Blinov, V. V. Kositsin, A. I. Lukyanchik
Format: Article
Language:English
Published: Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education 2023-03-01
Series:Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
Subjects:
autonomous heating element
propulsion system
small spacecraft
porous structure
design layout
specific heat capacity
resistojet
Online Access:https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2023/%D0%A2.7,%20%E2%84%961%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/55-60%20%20%D0%91%D0%BB%D0%B8%D0%BD%D0%BE%D0%B2%20%D0%92.%20%D0%9D.,%20%D0%9A%D0%BE%D1%81%D0%B8%D1%86%D1%8B%D0%BD%20%D0%92.%20%D0%92.,%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..pdf
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