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Understanding the decomposition of thermal protection systems is vital when designing hypersonic vehicles. This work shows that emission spectroscopy can be used to assess the accuracy of computational chemical models.
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This page is a summary of: Modeling of Emission Spectra in Nonequilibrium Plasmas for Testing Pyrolyzing Ablators, Journal of Thermophysics and Heat Transfer, October 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.t5615.
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