Numerical investigation of the effect of the configuration of ExoMars landing platform propulsion system on the interaction of supersonic jets with the surface of Mars

This paper presents the results of numerical investigations of the interaction with the Mars surface of four supersonic jets of ExoMars landing platform propulsion system. The cases of impingement of supersonic jets on a curved surface are considered depending on the values of propulsion system thru...

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Bibliographic Details
Published in:AIP Conference Proceedings Vol. 1893. P. 030084-1-030084-9
Other Authors: Kagenov, Anuar M, Kostyushin, Kirill V, Eremin, Ivan V, Shuvarikov, Vladimir, Glazunov, Anatoly A.
Format: Article
Language:English
Subjects:
Online Access:http://vital.lib.tsu.ru/vital/access/manager/Repository/vtls:000620550
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024 7 |a 10.1063/1.5007542  |2 doi 
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039 9 |a 201802200736  |c 201802011634  |d VLOAD  |y 201802011610  |z Александр Эльверович Гилязов 
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245 1 0 |a Numerical investigation of the effect of the configuration of ExoMars landing platform propulsion system on the interaction of supersonic jets with the surface of Mars  |c A. Kagenov, A. Glazunov, K. Kostyushin [et.al.] 
504 |a Библиогр.: 29 назв. 
520 3 |a This paper presents the results of numerical investigations of the interaction with the Mars surface of four supersonic jets of ExoMars landing platform propulsion system. The cases of impingement of supersonic jets on a curved surface are considered depending on the values of propulsion system thrust. According to the results of numerical studies are obtained the values of normal stresses on the surface of Mars at altitudes of 1.0, 0.5 and 0.3 meter to the surface of the landing. To define the occurring shear stresses Mohr-Coulomb theory was used. The maximum values of shear stresses were defined for the following types of soil of Mars: drift material, crusty to cloddy material, blocky material, sand and Mojave Mars simulant. The conducted evaluations showed, regardless of the propulsion system configuration, that when the final stage of the controlled landing of the ExoMars landing platform, the erosion of the Mars regolith would be insignificant. The estimates are consistent with the available data from previous Mars missions. 
653 |a сверхзвуковые струи 
653 |a Экзомарс, поверхностная платформа 
653 |a Марс, планета 
653 |a численные исследования 
653 |a Мора-Кулона теория 
653 |a сдвиговые напряжения 
653 |a силовые установки 
655 4 |a статьи в журналах  |9 879358 
700 1 |a Kagenov, Anuar M  |9 142519 
700 1 |a Kostyushin, Kirill V  |9 142520 
700 1 |a Eremin, Ivan V  |9 121414 
700 1 |a Shuvarikov, Vladimir  |9 142521 
700 1 |a Glazunov, Anatoly A.  |9 101551 
773 0 |t AIP Conference Proceedings  |d 2017  |g Vol. 1893. P. 030084-1-030084-9  |x 0094-243X 
852 4 |a RU-ToGU 
856 7 |u http://vital.lib.tsu.ru/vital/access/manager/Repository/vtls:000620550 
856 |y Перейти в каталог НБ ТГУ  |u https://koha.lib.tsu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=41571 
908 |a статья 
999 |c 41571  |d 41571