Thermodynamic properties of carbon–phenolic gas mixtures

James Scoggins, Jason Rabinovitch, Benjamin Barros-Fernandez, Alexandre Martin, Jean Lachaud, Richard Jaffe, Nagi Mansour, Guillaume Blanquart, Thierry Magin

Producción científica: Articlerevisión exhaustiva

28 Citas (Scopus)

Resumen

Accurate thermodynamic properties for species found in carbon–phenolic gas mixtures are essential in predicting material response and heating of carbon–phenolic heat shields of planetary entry vehicles. A review of available thermodynamic data for species found in mixtures of carbon–phenolic pyrolysis and ablation gases and atmospheres rich with C, H, O, and N such as those of Earth, Mars, Titan, and Venus, is performed. Over 1200 unique chemical species are identified from four widely used thermodynamic databases and a systematic procedure is described for combining these data into a comprehensive model. The detailed dataset is then compared with the Chemical Equilibrium with Applications thermodynamic database developed by NASA in order to quantify the differences in equilibrium thermodynamic properties obtained with the two databases. In addition, a consistent reduction methodology using the mixture thermodynamic properties as an objective function is developed to generate reduced species sets for a variety of temperature, pressure, and elemental composition spaces. It is found that 32 and 23 species are required to model carbon–phenolic pyrolysis gases mixed with air and CO2, respectively, to maintain a maximum error in thermodynamic quantities below 10%.

Idioma originalEnglish
Páginas (desde-hasta)177-192
Número de páginas16
PublicaciónAerospace Science and Technology
Volumen66
DOI
EstadoPublished - jul 1 2017

Nota bibliográfica

Publisher Copyright:
© 2017 Elsevier Masson SAS

Financiación

J.B.S., B.B.F., and T.E.M. were funded by the European Research Council Starting Grant #259354: “Multiphysics models and simulations for reacting and plasma flows applied to the space exploration program.” A.M. was supported through NASA Award NNX13AN04A. J.L. was funded by the NASA Space Technology Research Grants Program, grant NNX12AG47A. J.R. and G.B. were funded by the U.S. Air Force Office of Scientific Research, grant FA9550-12-1-0472. Finally, the authors wish to thank Prof. Burcat for his timely and helpful answers to our questions.

FinanciadoresNúmero del financiador
National Aeronautics and Space AdministrationNNX13AN04A, NNX12AG47A
Air Force Office of Scientific Research, United States Air ForceFA9550-12-1-0472
National Council for Eurasian and East European Research259354

    ASJC Scopus subject areas

    • Aerospace Engineering

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