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Blackout analysis of Mars entry missions

Published online by Cambridge University Press:  16 October 2020

Sahadeo Ramjatan Open the ORCID record for Sahadeo Ramjatan [Opens in a new window] ,
A. Lani Open the ORCID record for A. Lani [Opens in a new window] ,
S. Boccelli Open the ORCID record for S. Boccelli [Opens in a new window] ,
B. Van Hove ,
Ö. Karatekin Open the ORCID record for Ö. Karatekin [Opens in a new window] ,
T. Magin Open the ORCID record for T. Magin [Opens in a new window]  and
J. Thoemel Open the ORCID record for J. Thoemel [Opens in a new window]
Sahadeo Ramjatan*
Affiliation:
Aeronautics and Aerospace Department, von Karman Institute for Fluid Dynamics, Chaussée de Waterloo 72, 1640Rhode-Saint-Genèse, Belgium
A. Lani
Affiliation:
Aeronautics and Aerospace Department, von Karman Institute for Fluid Dynamics, Chaussée de Waterloo 72, 1640Rhode-Saint-Genèse, Belgium
S. Boccelli
Affiliation:
Aeronautics and Aerospace Department, von Karman Institute for Fluid Dynamics, Chaussée de Waterloo 72, 1640Rhode-Saint-Genèse, Belgium
B. Van Hove
Affiliation:
Aeronautics and Aerospace Department, von Karman Institute for Fluid Dynamics, Chaussée de Waterloo 72, 1640Rhode-Saint-Genèse, Belgium Royal Observatory of Belgium, Ringlaan 3, Brussels/Uccle1180, Belgium
Ö. Karatekin
Affiliation:
Royal Observatory of Belgium, Ringlaan 3, Brussels/Uccle1180, Belgium
T. Magin
Affiliation:
Aeronautics and Aerospace Department, von Karman Institute for Fluid Dynamics, Chaussée de Waterloo 72, 1640Rhode-Saint-Genèse, Belgium
J. Thoemel
Affiliation:
University of Luxembourg, 29, avenue J.F. Kennedy, L-1855, Luxembourg
*
†Email address for correspondence: [email protected]
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Abstract

A new methodology to accurately and efficiently examine the radio frequency blackout phenomenon during the hypersonic reentry process is introduced and validated. The current state-of-the-art thermochemical modelling of $\textrm {CO}_2$ flows is reviewed and one-dimensional stagnation line studies are performed in order to determine a suitable chemical mechanism for the electron density modelling. Hypersonic computational fluid dynamics (CFD) simulations are performed with a simplified chemical model including only neutral species, in order to calculate the flow field surrounding the ExoMars Schiapparelli module in flight conditions. A novel decoupled CFD approach is then applied where the calculation of the electron density is performed separately using a computationally inexpensive Lagrangian approach. Subsequently, a ray tracing algorithm is applied in order to model the propagation of electromagnetic waves in the wake flow past the ExoMars vehicle accounting for collisions between electrons and gas particles. The numerical results of the proposed novel approach for blackout analysis consisting of CFD, Lagrangian and ray tracing algorithms are in good agreement with the flight data.

JFM classification

Aerodynamics: High-speed flow Mathematical Foundations: Computational methods MHD and Electrohydrodynamics: Plasmas
Type
JFM Papers
Information
Journal of Fluid Mechanics , Volume 904 , 10 December 2020 , A26
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Copyright
© The Author(s), 2020. Published by Cambridge University Press

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References

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