@inproceedings{7aff307ce6bc46ae800d9146c885d64b,
title = "Comparison between traditional and competitive reaction models for the pyrolysis of high temperature aerospace materials",
abstract = "When carbon/phenolic ablators used as spacecraft heatshields are submitted to high temperatures, they undergo a series of irreversible chemical reactions in a process known as pyrolysis. This process has been modeled using different approaches depending on the application field. We compare two pyrolysis models: the traditional devolatilization and the competitive reaction model commonly adopted in the analysis of biomass. We discuss advantages and disadvantages of each approach and provide results on the pyrolysis modeling of the Phenolic Impregnated Carbon Ablator using each method.",
author = "Herrador, {F. Torres} and J. Coheur and T. Magin and J. Blondeau and J. Meurisse and F. Panerai and J. Lachaud and Mansour, {N. N.}",
note = "Publisher Copyright: {\textcopyright} 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA Aviation 2019 Forum ; Conference date: 17-06-2019 Through 21-06-2019",
year = "2019",
doi = "10.2514/6.2019-3361",
language = "English (US)",
isbn = "9781624105890",
series = "AIAA Aviation 2019 Forum",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
pages = "1--14",
booktitle = "AIAA Aviation 2019 Forum",
}