This paper represents an on-going effort at NASA Ames Research Center to develop a physics-based nonequilibrium model for hypersonic entry into the Martian atmosphere.
Development of a New Nonequilibrium Chemistry Model or Mars Entry
2017
24 pages
Report
No indication
English
Physical & Theoretical Chemistry , Physics , Astronautics , Mars atmosphere , Computational fluid dynamics , Atmospheric entry , Computational chemistry , Nonequilibrium conditions , Mars landing , Dissociation , Flow distribution , Mathematical models , Thermochemistry , Payloads , Potential energy , Hypersonics , Chemical reactions , Enthalpy , Entropy , Carbon monoxide , Argon , Carbon dioxide , Shock tubes , Heat transfer coefficients
On the Development of a New Nonequilibrium Chemistry Model for Mars Entry (AIAA 2017-1372)
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