Standard

Numerical simulation of hypervelocity impact problem for spacecraft shielding elements. / Silnikov, M.V.; Guk, I.V.; Nechunaev, A.F.; Smirnov, N.N.

в: Acta Astronautica, 31.08.2017, стр. Published online; .

Результаты исследований: Научные публикации в периодических изданияхстатьяРецензирование

Harvard

APA

Vancouver

Author

Silnikov, M.V. ; Guk, I.V. ; Nechunaev, A.F. ; Smirnov, N.N. / Numerical simulation of hypervelocity impact problem for spacecraft shielding elements. в: Acta Astronautica. 2017 ; стр. Published online; .

BibTeX

@article{0fa42853235c4bedade9fe27f8f83b60,
title = "Numerical simulation of hypervelocity impact problem for spacecraft shielding elements",
abstract = "The paper is aimed at modeling results of hypervelocity impact of space debris fragments on shielding elements of space structures. For this purpose we developed numerical model based on a smoothed particle hydrodynamics method. Verification and validation of the model was made in simulation of a process of a hypervelocity impact of a spherical projectile with a thin plate and comparison with experimental data. The calculations were performed using Ls-Dyna explicit software. Both experimental and calculated debris clouds show practically identical characters of their development, their propagation velocity, shape and size. Collisions of the thin plate with other types of projectiles - cubes with various spatial orientations, cylindrical projectile were considered and their peculiarities analyzed. It was shown, that in case of the cube sharp edge impact, a debris cloud of a higher density, and therefore most dangerous for the considered systems of two plates, is formed",
keywords = "Space debris, Collision, Space debris, Collision, Smoothed particle hydrodynamics method, Hypervelocity impact, Whipple shield",
author = "M.V. Silnikov and I.V. Guk and A.F. Nechunaev and N.N. Smirnov",
year = "2017",
month = aug,
day = "31",
doi = "10.1016/j.actaastro.2017.08.030",
language = "English",
pages = "Published online; ",
journal = "Acta Astronautica",
issn = "0094-5765",
publisher = "Elsevier",

}

RIS

TY - JOUR

T1 - Numerical simulation of hypervelocity impact problem for spacecraft shielding elements

AU - Silnikov, M.V.

AU - Guk, I.V.

AU - Nechunaev, A.F.

AU - Smirnov, N.N.

PY - 2017/8/31

Y1 - 2017/8/31

N2 - The paper is aimed at modeling results of hypervelocity impact of space debris fragments on shielding elements of space structures. For this purpose we developed numerical model based on a smoothed particle hydrodynamics method. Verification and validation of the model was made in simulation of a process of a hypervelocity impact of a spherical projectile with a thin plate and comparison with experimental data. The calculations were performed using Ls-Dyna explicit software. Both experimental and calculated debris clouds show practically identical characters of their development, their propagation velocity, shape and size. Collisions of the thin plate with other types of projectiles - cubes with various spatial orientations, cylindrical projectile were considered and their peculiarities analyzed. It was shown, that in case of the cube sharp edge impact, a debris cloud of a higher density, and therefore most dangerous for the considered systems of two plates, is formed

AB - The paper is aimed at modeling results of hypervelocity impact of space debris fragments on shielding elements of space structures. For this purpose we developed numerical model based on a smoothed particle hydrodynamics method. Verification and validation of the model was made in simulation of a process of a hypervelocity impact of a spherical projectile with a thin plate and comparison with experimental data. The calculations were performed using Ls-Dyna explicit software. Both experimental and calculated debris clouds show practically identical characters of their development, their propagation velocity, shape and size. Collisions of the thin plate with other types of projectiles - cubes with various spatial orientations, cylindrical projectile were considered and their peculiarities analyzed. It was shown, that in case of the cube sharp edge impact, a debris cloud of a higher density, and therefore most dangerous for the considered systems of two plates, is formed

KW - Space debris

KW - Collision

KW - Space debris

KW - Collision

KW - Smoothed particle hydrodynamics method

KW - Hypervelocity impact

KW - Whipple shield

UR - http://www.sciencedirect.com/science/article/pii/S0094576517311888

U2 - 10.1016/j.actaastro.2017.08.030

DO - 10.1016/j.actaastro.2017.08.030

M3 - Article

SP - Published online;

JO - Acta Astronautica

JF - Acta Astronautica

SN - 0094-5765

ER -

ID: 9056456