Email this article Numerical simulation of some problems of recovery capsule aerodynamics
- Authors: Belotserkovskii O.M.1, Babakov A.V.1, Beloshitskiy A.V.2, Gaydaenko V.I.1, Dyadkin A.A.2
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Affiliations:
- Institute of Computer-Aided Design (ICAD)
- Korolev Rocket and Space Public Corporation Energia (RSC Energia)
- Issue: Vol 8, No 5 (2016)
- Pages: 568-576
- Section: Article
- URL: https://journals.rcsi.science/2070-0482/article/view/201229
- DOI: https://doi.org/10.1134/S2070048216050057
- ID: 201229
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Abstract
This paper presents the numerical simulation of the circumfluence of a recovery apparatus with brake engines and a detachable heat protection shield carried out by the use of the conservative numerical method of cluster architecture. The simulation results of the action of reactive jets of brake engines on the landing surface and the recovery apparatus, as well as the basic aerodynamic characteristics, are considered.
About the authors
O. M. Belotserkovskii
Institute of Computer-Aided Design (ICAD)
Email: icad@icad.org.ru
Russian Federation, Moscow
A. V. Babakov
Institute of Computer-Aided Design (ICAD)
Author for correspondence.
Email: icad@icad.org.ru
Russian Federation, Moscow
A. V. Beloshitskiy
Korolev Rocket and Space Public Corporation Energia (RSC Energia)
Email: icad@icad.org.ru
Russian Federation, Moscow
V. I. Gaydaenko
Institute of Computer-Aided Design (ICAD)
Email: icad@icad.org.ru
Russian Federation, Moscow
A. A. Dyadkin
Korolev Rocket and Space Public Corporation Energia (RSC Energia)
Email: icad@icad.org.ru
Russian Federation, Moscow
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