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Basic aspects of topological technology of automated on-board equipment layout in space vehicle compartments using the example of “Yantar-2k” Earth remote sensing space vehicle
- Authors: Belyakov A.A.1, Shulepov A.I.1
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Affiliations:
- Samara National Research University
- Issue: Vol 21, No 4 (2022)
- Pages: 7-24
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/11041
- DOI: https://doi.org/10.18287/2541-7533-2022-21-4-7-24
- ID: 11041
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Abstract
The article presents the theoretical foundations of automated design of on-board equipment layout in spacecraft compartments in terms of topology. The purpose of the work is to create a flexible arrangement model that would allow solving the problem for any configuration of the structure, taking into account the engineering and operational restrictions imposed on the objects located in a limited space. The technology is formalized according to the methods of the foundations of topology and in this work is demonstrated for a two-dimensional case by comparing it with a reference design-layout scheme. The functional, installation, dimensional, thermal, vibroacoustic requirements are taken into account with the mass-centering restrictions of the layout. In the course of the study, a new approach to describing the design process of assembling on-board equipment was obtained, which can be fully digitized and then integrated into known computer-aided design systems. It has been verified using the example of the power supply system of the “Yantar-2k” spacecraft.
About the authors
A. A. Belyakov
Samara National Research University
Author for correspondence.
Email: jake.dunn@inbox.ru
ORCID iD: 0000-0002-5789-8048
Student
Russian FederationA. I. Shulepov
Samara National Research University
Email: shulepov-al@mail.ru
Candidate of Science (Engineering), Associate Professor of the Department of Space Engineering
Russian FederationReferences
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