TRANSPORT TECHNICS. INVESTIGATION OF ELEMENTS. RELIABILITY

Modelling of Spacecraft Operating Conditions During Off-Nominal Situations in Orbit and Analysis of Acoustic Emission Monitoring Parameters for Their Optimisation

  • 1 Head of the non-destructive testing laboratory, Leading Researcher: Institute of Aeronautics, Space Engineering and Transport of Riga Technical University, Riga, Latvia.
  • 2 Vice President ScientificTehnical Union of Mechanical Engineering “INDUSTRY – 4.0”, Sofia, Bulgaria
  • 3 Leading Researcher at the Laboratory of Non-Destructive Testing, Institute of Aeronautics, Space Engineering and Transport of Riga Technical University, Riga, Latvia. Riga, Latvia
  • 4 Scientific Researcher of the laboratory of non-destructive testing: Institute of Aeronautics, Space Engineering and Transport of Riga Technical University., Riga, Latvia
  • 5 Scientific assistant: Institute of Aeronautics, Space Engineering and Transport of Riga Technical University, Riga, Latvia

Abstract

The subject of the article is the planning and comprehensive preparation of an experiment for monitoring the condition of a satellite’s structure under vacuum conditions modelled using a space environment simulator. Simulating the space environment is essential for verifying the performance of materials, structural components and equipment prior to their actual launch. Such testing makes it possible to confirm the correctness of material selection, the accuracy of engineering calculations and the validity of technical decisions made during the design phase. The behaviour of materials under vacuum, extreme temperatures, sharp thermal fluctuations, and exposure to cosmic radiation may differ significantly from their performance under standard operating conditions on Earth.

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References

  1. M.Banov, D.Troyenkin, А.Urbahs, S.Minatsevich, Aeroengine gas turbine blades’ condition monitoring by acoustic emission method, Defectoscopy, 1986, № 9, p. 58-63
  2. А.Н. Серьезнов, Л.Н. Степанова, С.И. Кабанов, А.Е. Кареев, Е.Ю. Лебедев, В.Л. Кожемякин, И.С. Рамазанов и др.; под ред. Л.Н. Степановой, А.Н. Серьезнова. Акустико-эмиссионный контроль авиационных конструкций /– М.: Машиностроение / Машиностроение-Полет, 2008. – 440 с.
  3. А.Shanyavsky, М.Banov, Т.Zakharova. Principles of physical mezomechanics at nanostructural level of fatigue in metals. Part 1. Fatigue cracks’ origin model in titanium alloy VT3-1 under surface. / Physical mezomechanics, 2010 vol. 13 - №1. -p. 61-72
  4. Vinogradov, L., Kuļešovs, N., Dolgov, N., Smirnov, I., Šestakovs, V. Experimental and Statistical Study of In- Plane Tensile and Adhesion Strength of Plasma- Sprayed Coatings. Applied Mechanics and Materials, 2020, Vol. 897, 61.-67.lpp. ISSN 1662-7482.
  5. Vinogradov L., Strautmanis G., Gutans J., Soldatova Y.,Prokopenko V., Development of an acoustic emission signal recording system. Scientific-Technical Union of Mechanical Engineering the XXXIII International Scientific Conference „trans&MOTAUTO'25” 23– 26.06.2025 Varna, Bulgaria
  6. BS EN 13554:2011 Non-destructive testing. Acoustic emission testing. General principles (British Standard)

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