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Emission Spectroscopic Boundary Layer Investigation during Ablative Material Testing in Plasmatron

Ablative Thermal Protection Systems (TPS) allowed the first humans to safely return to Earth from the moon and are still considered as the only solution for future high-speed reentry missions. But despite the advancements made since Apollo, heat flux prediction remains an imperfect science and engin...

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Autores principales: Helber, Bernd, Chazot, Olivier, Hubin, Annick, Magin, Thierry E.
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MyJove Corporation 2016
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4927775/
https://www.ncbi.nlm.nih.gov/pubmed/27340820
http://dx.doi.org/10.3791/53742
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author Helber, Bernd
Chazot, Olivier
Hubin, Annick
Magin, Thierry E.
author_facet Helber, Bernd
Chazot, Olivier
Hubin, Annick
Magin, Thierry E.
author_sort Helber, Bernd
collection PubMed
description Ablative Thermal Protection Systems (TPS) allowed the first humans to safely return to Earth from the moon and are still considered as the only solution for future high-speed reentry missions. But despite the advancements made since Apollo, heat flux prediction remains an imperfect science and engineers resort to safety factors to determine the TPS thickness. This goes at the expense of embarked payload, hampering, for example, sample return missions. Ground testing in plasma wind-tunnels is currently the only affordable possibility for both material qualification and validation of material response codes. The subsonic 1.2MW Inductively Coupled Plasmatron facility at the von Karman Institute for Fluid Dynamics is able to reproduce a wide range of reentry environments. This protocol describes a procedure for the study of the gas/surface interaction on ablative materials in high enthalpy flows and presents sample results of a non-pyrolyzing, ablating carbon fiber precursor. With this publication, the authors envisage the definition of a standard procedure, facilitating comparison with other laboratories and contributing to ongoing efforts to improve heat shield reliability and reduce design uncertainties. The described core techniques are non-intrusive methods to track the material recession with a high-speed camera along with the chemistry in the reactive boundary layer, probed by emission spectroscopy. Although optical emission spectroscopy is limited to line-of-sight measurements and is further constrained to electronically excited atoms and molecules, its simplicity and broad applicability still make it the technique of choice for analysis of the reactive boundary layer. Recession of the ablating sample further requires that the distance of the measurement location with respect to the surface is known at all times during the experiment. Calibration of the optical system of the applied three spectrometers allowed quantitative comparison. At the fiber scale, results from a post-test microscopy analysis are presented.
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spelling pubmed-49277752016-07-12 Emission Spectroscopic Boundary Layer Investigation during Ablative Material Testing in Plasmatron Helber, Bernd Chazot, Olivier Hubin, Annick Magin, Thierry E. J Vis Exp Engineering Ablative Thermal Protection Systems (TPS) allowed the first humans to safely return to Earth from the moon and are still considered as the only solution for future high-speed reentry missions. But despite the advancements made since Apollo, heat flux prediction remains an imperfect science and engineers resort to safety factors to determine the TPS thickness. This goes at the expense of embarked payload, hampering, for example, sample return missions. Ground testing in plasma wind-tunnels is currently the only affordable possibility for both material qualification and validation of material response codes. The subsonic 1.2MW Inductively Coupled Plasmatron facility at the von Karman Institute for Fluid Dynamics is able to reproduce a wide range of reentry environments. This protocol describes a procedure for the study of the gas/surface interaction on ablative materials in high enthalpy flows and presents sample results of a non-pyrolyzing, ablating carbon fiber precursor. With this publication, the authors envisage the definition of a standard procedure, facilitating comparison with other laboratories and contributing to ongoing efforts to improve heat shield reliability and reduce design uncertainties. The described core techniques are non-intrusive methods to track the material recession with a high-speed camera along with the chemistry in the reactive boundary layer, probed by emission spectroscopy. Although optical emission spectroscopy is limited to line-of-sight measurements and is further constrained to electronically excited atoms and molecules, its simplicity and broad applicability still make it the technique of choice for analysis of the reactive boundary layer. Recession of the ablating sample further requires that the distance of the measurement location with respect to the surface is known at all times during the experiment. Calibration of the optical system of the applied three spectrometers allowed quantitative comparison. At the fiber scale, results from a post-test microscopy analysis are presented. MyJove Corporation 2016-06-09 /pmc/articles/PMC4927775/ /pubmed/27340820 http://dx.doi.org/10.3791/53742 Text en Copyright © 2016, Journal of Visualized Experiments http://creativecommons.org/licenses/by-nc-nd/3.0/ This is an open-access article distributed under the terms of the Creative Commons Attribution-NonCommercial-NoDerivs 3.0 Unported License. To view a copy of this license, visithttp://creativecommons.org/licenses/by-nc-nd/3.0/
spellingShingle Engineering
Helber, Bernd
Chazot, Olivier
Hubin, Annick
Magin, Thierry E.
Emission Spectroscopic Boundary Layer Investigation during Ablative Material Testing in Plasmatron
title Emission Spectroscopic Boundary Layer Investigation during Ablative Material Testing in Plasmatron
title_full Emission Spectroscopic Boundary Layer Investigation during Ablative Material Testing in Plasmatron
title_fullStr Emission Spectroscopic Boundary Layer Investigation during Ablative Material Testing in Plasmatron
title_full_unstemmed Emission Spectroscopic Boundary Layer Investigation during Ablative Material Testing in Plasmatron
title_short Emission Spectroscopic Boundary Layer Investigation during Ablative Material Testing in Plasmatron
title_sort emission spectroscopic boundary layer investigation during ablative material testing in plasmatron
topic Engineering
url https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4927775/
https://www.ncbi.nlm.nih.gov/pubmed/27340820
http://dx.doi.org/10.3791/53742
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