Journal article
Reconstruction of Mars 2020 backshell radiative heating via infrared emission spectroscopy of CO2/N2/Ar shockwaves
- Abstract:
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A test series was performed in the Electric Arc Shock Tube (EAST) facility with the aim of reproducing flight conditions encountered during the Mars 2020 mission entry into the Mars atmosphere. For this test series, the EAST facility was instrumented with two spectrometers for optical emission spectroscopy (OES) measurements and three mid-infrared lasers for tunable diode laser absorption spectroscopy (TDLAS). This paper focuses on the spectrally and spatially resolved radiance measured with OES. Conditions were chosen to achieve similarity to backshell radiative heating measured with the MEDLI2 heat flux gauges near and after the time of peak heating. Comparisons were made against two candidate kinetic models for Mars entry. Below 2.7 km/s, the chemistry is effectively frozen, with measurements being above both models and CEA predictions. It is shown that taking into account shock deceleration in the tube explains most of the discrepancy between measured and frozen radiance. For velocities above 2.7 km/s, the data lies between the two models. However, adjusting for shock deceleration indicates that one of the models may be preferred for predicting CO2 dissociation. Finally, comparisons between OES and TDLAS data are made and show a good agreement on the measured temperature and CO2 number density profiles, typically within 10 and 5%, respectively. A good agreement is also observed for the radiance that would be inferred based upon the quantities measured by TDLAS.
- Publication status:
- Published
- Peer review status:
- Peer reviewed
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- Files:
-
-
(Preview, Accepted manuscript, pdf, 4.2MB, Terms of use)
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- Publisher copy:
- 10.2514/1.t6916
Authors
- Publisher:
- American Institute of Aeronautics and Astronautics
- Journal:
- Journal of Thermophysics and Heat Transfer More from this journal
- Volume:
- 38
- Issue:
- 4
- Pages:
- 568-585
- Publication date:
- 2024-08-09
- Acceptance date:
- 2024-03-13
- DOI:
- EISSN:
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1533-6808
- ISSN:
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0887-8722
- Language:
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English
- Keywords:
- Pubs id:
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2022192
- Local pid:
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pubs:2022192
- Deposit date:
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2025-10-24
Terms of use
- Copyright holder:
- American Institute of Aeronautics and Astronautics, Inc.
- Copyright date:
- 2024
- Rights statement:
- Copyright © 2024 by the American Institute of Aeronautics and Astronautics, Inc.
- Notes:
- This is the accepted manuscript version of the article. The final version is available online from American Institute of Aeronautics and Astronautics at https://dx.doi.org/10.2514/1.t6916
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