Investigation of the dynamics of the movement of space descent vehicles in the atmosphere of the planet using modern means of mathematical modeling

For reentry in Mars atmosphere, inflatable braking devices are interesting as they do not use rigid heat shields, parachutes, or retrorockets which limits the mass to send into space. This paper focuses on one MetNet probe, to validate the use of inflatable braking device geometry. This study shows...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Koryanov, Vsevolod V., Menetrier–Hacquemand, Nathan
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Aerodynamic coefficients Atmospheric entry Braking Deformation effects Heat shields Mars atmosphere Mars surface Planetary atmospheres
Online-Zugang:	Volltext
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