Computational Aerothermodynamic Environments for the Mars 2020 Entry Capsule

Abstract

The simulation tools and processes used to generate aerothermodynamic environment definitions for the Mars 2020 entry capsule are presented. The Mars 2020 capsule leverages the heritage Mars Science Laboratory design, but the entry will follow a different trajectory, landing at a different location and altitude onMars. The general strategy for creating theMars 2020mission-specific environments follows from theMars Science Laboratory experience. The primary difference is that now the effects of shock-layer radiation are modeled, with particular concern for the backshell.