Email this article Study of Aerodynamics of a Prospective Descent Module Descending in the Atmosphere of Mars
- Authors: Golomazov M.M.1, Ivankov A.A.2
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Affiliations:
- Institute for Computer-Aided Design, Russian Academy of Sciences
- Lavochkin Association
- Issue: Vol 53, No 7 (2019)
- Pages: 500-505
- Section: Article
- URL: https://journal-vniispk.ru/0038-0946/article/view/171443
- DOI: https://doi.org/10.1134/S0038094619070098
- ID: 171443
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Abstract
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.
About the authors
M. M. Golomazov
Institute for Computer-Aided Design, Russian Academy of Sciences
Author for correspondence.
Email: mmg@icad.org.ru
Russian Federation, Moscow
A. A. Ivankov
Lavochkin Association
Author for correspondence.
Email: ival@laspace.ru
Russian Federation, Khimki, Moscow oblast, 141402
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