Theoretical and experimental study of a method for the protection of spacecraft from high–speed particles

In this paper, we perform numerical simulation and experimental determination of the limiting resistance of the spacecraft design elements used when developing anti-meteorite protection of spacecraft as well as protection against space debris. One possible way to increase the efficiency of protectiv...

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Veröffentlicht in:	Cosmic research 2016-03, Vol.54 (2), p.118-126
Hauptverfasser:	Gerasimov, A. V., Dobritsa, D. B., Pashkov, S. V., Khristenko, Yu. F.
Format:	Artikel
Sprache:	eng
Schlagworte:	Astronomy Astrophysics and Astroparticles Astrophysics and Cosmology Computer simulation Constraining Finite element method High speed Mathematical models Numerical simulations Physics Physics and Astronomy Shields Space debris Space Exploration and Astronautics Space Sciences (including Extraterrestrial Physics Spacecraft Spacecraft design
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Zusammenfassung:	In this paper, we perform numerical simulation and experimental determination of the limiting resistance of the spacecraft design elements used when developing anti-meteorite protection of spacecraft as well as protection against space debris. One possible way to increase the efficiency of protective shields and satisfy the requirements of the mass characteristics of the latter is the use of mesh barriers.
ISSN:	0010-9525 1608-3075
DOI:	10.1134/S0010952516020015