Radiative Heating Uncertainty for Hyperbolic Earth Entry, Part 1: Flight Simulation Modeling and Uncertainty

This paper investigates the shock-layer radiative heating uncertainty for hyperbolic Earth entry, with the main focus being a Mars return. A baseline simulation approach involving the Laura Navier-Stokes code with coupled ablation and radiation is presented, with the Hara radiation code being used f...

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Veröffentlicht in:	Journal of spacecraft and rockets 2013-01, Vol.50 (1), p.19-38
Hauptverfasser:	Johnston, Christopher O, Mazaheri, Alireza, Gnoffo, Peter, Kleb, Bil, Bose, Deepak
Format:	Artikel
Sprache:	eng
Schlagworte:	Ablation Computer simulation Earth Flight simulation Heating Mars Mathematical models Navier-Stokes equations Uncertainty
Online-Zugang:	Volltext
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