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Solar System Research

, Volume 52, Issue 7, pp 578–589 | Cite as

Software Package for the Development of Thermal Protection Systems for Spacecraft Descent into the Atmospheres of Planets

  • M. M. GolomazovEmail author
  • A. A. Ivankov
Article
  • 8 Downloads

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.

Keywords

programming and computing suite descent module thermal protection trajectory heat transfer 

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Copyright information

© Pleiades Publishing, Inc. 2018

Authors and Affiliations

  1. 1.Institute of Computer-Aided DesignRussian Academy of SciencesMoscowRussia
  2. 2.Lavochkin AssociationKhimkiRussia

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