Autonomous experimental studies resistojet with two autonomous heating elements for nanosatellites
https://doi.org/10.25206/2588-0373-2023-7-4-48-55
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.
About the Authors
V. N. Blinov
Omsk State Technical University
Russian Federation
Russian Federation
BLINOV Viktor Nikolayevich, Doctor of Technical Sciences, Professor of Aircraft and Rocket Building Department
Omsk, Mira Ave., 11, 644050
V. V. Kositsyn
Omsk State Technical University
Russian Federation
Russian Federation
KOSITSIN Valeriy Vladimirovich, Candidate of Technical Sciences, Associate Professor of Aircraft and Rocket Building Department
Omsk, Mira Ave., 11, 644050
A. I. Lukyanchik
Omsk State Technical University
Russian Federation
Russian Federation
LUKYANCHIK Anton Igorevich, Senior Lecturer of Aircraft and Rocket Building Department
Omsk, Mira Ave., 11, 644050
P. V. Stepen
Omsk State Technical University
Russian Federation
Russian Federation
STEPEN Pavel Valeryevich, Senior Lecturer of Aircraft and Rocket Building Department
Omsk, Mira Ave., 11, 644050
P. S. Yachmenev
Omsk State Technical University
Russian Federation
Russian Federation
YACHMENEV Pavel Sergeyevich, Senior Lecturer of Aircraft and Rocket Building Department
Omsk, Mira Ave., 11, 644050
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Review
For citations:
Blinov V.N., Kositsyn V.V., Lukyanchik A.I., Stepen P.V., Yachmenev P.S. Autonomous experimental studies resistojet with two autonomous heating elements for nanosatellites. Omsk Scientific Bulletin. Series Aviation-Rocket and Power Engineering. 2023;7(4):48-55. (In Russ.) https://doi.org/10.25206/2588-0373-2023-7-4-48-55
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