The method of investigation of basic project parameters of microsatellite by random search

Authors

DOI:

https://doi.org/10.25206/2588-0373-2019-3-2-95-102

Keywords:

adapter, small spacecraft, small upper stage, basic design parameters, random search method

Abstract

A significant number of the main design parameters of the small upper stage for the group launch of small spacecraft with a propulsion system with a displacement fuel supply system determines the relevance of the random search method. The aim of the work is to create a method of selecting the main design parameters of the small upper stage by random search. The mathematical model based on the dimensional-mass model of the calculated mass determination provides the choice of the optimal mass of the upper stage, taking into account the complex relationships of the studied parameters.

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Author Biographies

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

Doctor of Technical Sciences, Professor of Aviation and Rocketry (AVIRS) Department.

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

Graduate Student, Assistant of AVIRS Department.

Viktor Vladimirovich Shalay, Omsk State Technical University, Omsk, Russia

Doctor of Technical, Sciences, Professor, Head of Oil and Gas Engineering, Standardization and Metrology Department, President of OmSTU.

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Abstract views: 13

Published

2019-06-25

How to Cite

Blinov В. Н., Lukyanchik А. И., & Shalay В. В. (2019). The method of investigation of basic project parameters of microsatellite by random search. Omsk Scientific Bulletin. Series «Aviation-Rocket and Power Engineering», 3(2), 95–102. https://doi.org/10.25206/2588-0373-2019-3-2-95-102

Issue

Vol. 3 No. 2 (2019)

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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