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Improved Chemistry and Attenuation Models for Communication Blackout Simulation During Mars 2020 EntryAs a blunt body enters a planetary atmosphere, a plasma forms in the hypersonic shock layer and attenuates radio communication causing signal blackout for some duration of the entry sequence. In our previous work,1 computational fluid dynamics (CFD) was applied to model the entry flow around the Mars 2020 spacecraft, including ionization and electron density throughout the flow field, and predict ultra-high frequency (UHF) radio wave attenuation due to electrons. In total, 17 chemical species and their spatial profiles are modelled around the Mars 2020 spacecraft at 11 different points in time during entry. Although the simulation predicted the onset of attenuation well, the timing of the end of the predicted blackout window significantly preceded the end time observed during the 2021 landing. The present work seeks to improve the attenuation model by accounting for the fact that electrons undergo collisions with heavier species in the flow, which is an effect that was neglected in previous analyses. It is determined that including electron collisions increases the overall magnitude of attenuation predicted especially towards the end of the measured attenuation period, improving qualitative agreement between predicted and measured attenuation to both spacecraft receiving the signal from Mars 2020. To explore the remaining uncertainty in signal attenuation predictions further, a sensitivity study is performed to investigate the impact of associative ionization and electron-impact ionization rate coefficients on the electron density predicted by CFD and on the resulting attenuation predictions. These coefficients are believed to contain up to order-of-magnitude uncertainty, and therefore may significantly affect the number density of electrons throughout the flow field. Variations in associative ionization coefficients demonstrate significant impact on the magnitude of attenuation due to variation in the electron density coming from associative ionization. However, the start and end times of the predicted signal attenuation period are only slightly impacted by said variation.
Document ID
20240000251
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Eve Papajak
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Trevor Hedges
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Christopher Naughton
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
David Saunders
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Date Acquired
January 8, 2024
Publication Date
January 10, 2024
Publication Information
Subject Category
Aerodynamics
Chemistry and Materials (General)
Meeting Information
Meeting: AIAA Science and Technology Forum and Exposition (2024 AIAA SciTech Forum)
Location: Orlando, FL
Country: US
Start Date: January 8, 2024
End Date: January 12, 2024
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
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