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Calculation and design of the main equipment for mobile space simulation system

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
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.
Rocznik
Strony
71--89
Opis fizyczny
Bibliogr. 20 poz., fot., rys., wzory
Twórcy
  • Institute of Aeronautics, Department of Civil and Mechanical Engineering of Riga Technical University, 6B Kipsalas Street, Riga, LV-1048, Latvia
autor
  • Institute of Aeronautics, Department of Civil and Mechanical Engineering of Riga Technical University, 6B Kipsalas Street, Riga, LV-1048, Latvia
  • Institute of Aeronautics, Department of Civil and Mechanical Engineering of Riga Technical University, 6B Kipsalas Street, Riga, LV-1048, Latvia
  • Department of Mechatronics and Armament, Kielce University of Technology, Tysiąclecia Państwa Polskiego 7 Street, 25-314 Kielce, Poland
Bibliografia
  • [1] Setlak L., Kowalik R., Lusiak T. Practical use of composite materials used in military aircraft. Materials [Internet]. 2021;14(17):4812. Available from: https://doi.org/10.3390/ma14174812
  • [2] Ley W., Wittmann K., Hallmann W. Handbook of space technology, 1st edn. Chichester: John Wiley & Sons Ltd; 2009.
  • [3] Kravchenko S., Panova N., Kuļešovs N., Blumbergs I., Šestakovs V. Analysis of the technical implementation options for launching a carrier for output of micro satellites to LEO from an aircraft platform (latlaunch project). In: Riga Technical University 61st International Scientific Conference, 2020 Oct 15-16; Rīga, Latvia. Rīga: RTU Press; 2020. p. 16-7.
  • [4] ASTM. C177-19 standard. Test method for steady-state heat flux measurements and thermal transmission properties by means of the guarded-hot-plate apparatus [Internet]. Available from: https://doi.org/10.1520/C0177-19
  • [5] EN 12667:2001 standard. Thermal performance of building materials and products - Determination of thermal resistance by means of guarded hot plate and heat flow meter methods - Products of high and medium thermal resistance. [place, publisher, date unknown].
  • [6] Mobile test stand PV 1236 [Internet]. Available from: https://www.irimex.ru/services/catalog/armatura/rubric_%20501/rubric_510/product_1651/.
  • [7] Mobile space environment testing equipment development of "Metamorphosis" prototype for transportation intermodal traffic [Internet]. Riga Technical University (Leading Partner), “CRYOGENIC AND VACUUM SYSTEMS” Ltd; 2022. Project 1.1.1.1/18/A/133. Available from: https://www.rtu.lv/en/university/rtu-projects/open?project_number=4127
  • [8] SIA “Cryogenic and vacuum systems.” [Internet]. European Space Agency; 2014. Available from: https://www.izm.gov.lv/sites/izm/files/latvian-entries1.pdf
  • [9] NASA systems engineering handbook (NASA/SP-2016-6105). Rev 2. Create space independent publishing platform. USA: NASA; 2017.
  • [10] Pisacane V. Fundamentals of space systems, 2nd edn. New York: Oxford University Press; 2005.
  • [11] Gilmore D. Spacecraft thermal control handbook - volume I: fundamental technologies, 2nd edn. California: The Aerospace Press; 2002.
  • [12] Kolaini A., Tsuha W., Fernandez J. Spacecraft vibration testing: benefits and potential issues. Adv Aircr Spacecr Sci [Internet]. 2018;5(2):165-75. Available from: https://doi.org/10.12989/aas.2018.5.2.165.
  • [13] European Cooperation for Space Standardization. ECSS-E-ST-10-03C. Space Engineering. Testing. ECSS Secretariat ESA-ESTEC Requirements & Standards Division Noordwijk. The Netherlands: 2012.
  • [14] NASA Goddard Space Flight Center. GSFC-STD-7000. General Environmental Verification Standard (GEVS) for GSFC Flight Programs and Projects. Maryland: NASA; 2013.
  • [15] International Standard Organization. ISO 17851:2016. Space systems - Space environment simulation for material tests - General principles and criteria. Geneva, Switzerland: ISO; 2016.
  • [16] Kravchenko S., Panova N., Cēbere M. METAMORPHOSIS - the space testing facility from ventspils. In: Space Research Review: Dedicated to the 25th anniversary of the Ventspils International Radio Astronomy Centre. Vol.5; 2017 Aug 23-24; Ventspils, Latvia. Ventspils University of Applied Sciences; 2018. p. 98-105.
  • [17] International Standard Organization. ISO 16528-1:2007. Boilers and pressure vessels. - Part 1: Performance requirements.
  • [18] International Standard Organization. ISO 16528-2:2007. Boilers and pressure vessels - Part 2: Procedures for fulfilling the requirements of ISO 16528-1.
  • [19] Volumetric and mass flow of gas [Internet]. Available from: https://www.massflow.ru/info/obemnyy-i-massovyy-rashod-gaza/.
  • [20] Chisabas R., Loureiro G., Lino CD. Space thermal and vacuum environment simulation. In: Dekoulis G, editor. Space flight [Internet]. InTech; 2018. Available from: https://doi.org/10.5772/intechopen.73154
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-8388e6e8-c977-4d34-b7de-5008731a9c54
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