Enviar artigo por via de e-mail Study of Aerodynamics of a Prospective Descent Module Descending in the Atmosphere of Mars
- Autores: Golomazov M.M.1, Ivankov A.A.2
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Afiliações:
- Institute for Computer-Aided Design, Russian Academy of Sciences
- Lavochkin Association
- Edição: Volume 53, Nº 7 (2019)
- Páginas: 500-505
- Seção: Article
- URL: https://journals.rcsi.science/0038-0946/article/view/171443
- DOI: https://doi.org/10.1134/S0038094619070098
- ID: 171443
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Resumo
The paper presents the methods and the calculation results for the flow around a prospective descent module and physicochemical processes in the flow field near the vehicle in the aerodynamic braking mode in the Martian atmosphere. The boundary conditions and the models of chemical processes corresponding to the actual conditions of entering the planet’s atmosphere are investigated.
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Sobre autores
M. Golomazov
Institute for Computer-Aided Design, Russian Academy of Sciences
Autor responsável pela correspondência
Email: mmg@icad.org.ru
Rússia, Moscow
A. Ivankov
Lavochkin Association
Autor responsável pela correspondência
Email: ival@laspace.ru
Rússia, Khimki, Moscow oblast, 141402
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