Autonomous experimental studies resistojet with two autonomous heating elements for nanosatellites

Authors

DOI:

https://doi.org/10.25206/2588-0373-2023-7-4-48-55

Keywords:

nanosatellite, propulsion system, resistojet, autonomous experimental research, autonomous heating element

Abstract

The purpose of the work is to conduct autonomous experimental studies of an resistojet with two
autonomous heating elements with a diameter of 4 mm. As a result of experimental studies of the
resistojet, the heating dynamics of the micromotor structure and the working fluid (isobutane) in the
power range from 5 W to 60 W is determined. Experimental studies have shown the possibility of using
the proposed resistojet design with two autonomous heating elements not only on small spacecraft, but
also on micro- and nanosatellites under conditions of limited on-board energy.

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Author Biographies

Blinov Viktor Nikolayevich, Omsk State Technical University, Omsk, Russia

Doctor of Technical Sciences, Professor of Aircraft and Rocket Building Department, Omsk State Technical University (OmSTU), Omsk.

Kositsyn Valeriy Vladimirovich, Omsk State Technical University, Omsk, Russia

Candidate of Technical Sciences, Associate Professor of Aircraft and Rocket Building Department, OmSTU, Omsk.

Lukyanchik Anton Igorevich, Omsk State Technical University, Omsk, Russia

Senior Lecturer of Aircraft and Rocket Building Department, OmSTU, Omsk.

Stepen Pavel Valeryevich, Omsk State Technical University, Omsk, Russia

Senior Lecturer of Aircraft and Rocket Building Department, OmSTU, Omsk.

Yachmenev Pavel Sergeevich, Omsk State Technical University, Omsk, Russia

Senior Lecturer of Aircraft and Rocket Building Department, OmSTU, Omsk.

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Abstract views: 14

Published

2023-12-22

How to Cite

Blinov В. Н., Kositsyn В. В., Lukyanchik А. И., Stepen П. В., & Yachmenev П. С. (2023). Autonomous experimental studies resistojet with two autonomous heating elements for nanosatellites. Omsk Scientific Bulletin. Series «Aviation-Rocket and Power Engineering», 7(4), 48–55. https://doi.org/10.25206/2588-0373-2023-7-4-48-55

Issue

Vol. 7 No. 4 (2023)

Section

Aviation and rocket-space engineering

License

Non-exclusive rights to the article are transferred to the journal in full accordance with the Creative Commons License BY-NC-SA 4.0 «Attribution-NonCommercial-ShareAlike 4.0 Worldwide License (CC BY-NC-SA 4.0»)

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