Email this article Software Package for the Development of Thermal Protection Systems for Spacecraft Descent into the Atmospheres of Planets
- Authors: Golomazov M.M.1, Ivankov A.A.2
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Affiliations:
- Institute of Computer-Aided Design
- Lavochkin Association
- Issue: Vol 52, No 7 (2018)
- Pages: 578-589
- Section: Article
- URL: https://journals.rcsi.science/0038-0946/article/view/171133
- DOI: https://doi.org/10.1134/S0038094618070109
- ID: 171133
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Abstract
The paper presents a mathematical model and a computational algorithm and describes a programming and computing suite (PCS) for the development of thermal protection systems for spacecraft designed to descend into the atmospheres of planets. The mathematical model and the PCS are implemented based on the development of thermal protection for the descent module of the EXOMARS 2020 surface platform.
About the authors
M. M. Golomazov
Institute of Computer-Aided Design
Author for correspondence.
Email: mmg@icad.org.ru
Russian Federation, Moscow
A. A. Ivankov
Lavochkin Association
Email: mmg@icad.org.ru
Russian Federation, Khimki
