Calculation and Design of the Main Equipment for Mobile Space Simulation System

Author:

Mozga Natalija1ORCID,Gutans Juris1ORCID,Kubulins Raivis1ORCID,Chatys Rafał2ORCID

Affiliation:

1. Institute of Aeronautics, Department of Civil and Mechanical Engineering of Riga Technical University , 6B Kipsalas Street , Riga , , Latvia

2. Department of Mechatronics and Armament, Kielce University of Technology , Tysiąclecia Państwa Polskiego 7 Street , Kielce , Poland

Abstract

ABSTRACT This article presents the results of the analysis of approaches to designing a mobile vacuum system ‘METAMORPHOSIS’ for simulation of space environment, which could help provide services of testing space objects at the request of the customers at a place and time acceptable to them, which allows saving time and assets in the development of space objects, their elements, including satellites. As a result of the conducted analysis, methodological approaches to the determination of the structure of the vacuum system were undertaken. To avoid unanticipated issues and to validate computer-driven modelling, testing in a space simulation chamber is an important part of the quality-assurance process. Spacecraft and their components must withstand extreme temperatures and pressure to travel outside the Earth’s atmosphere. Space simulation testing involves the use of a thermal vacuum chamber to replicate the conditions experienced in space.

Publisher

Walter de Gruyter GmbH

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