Conversion of hydrocarbon fuel in elements of thermal protection of a hypersonic flight vehicle
- Autores: Kuranov A.L.1, Korabel’nikov A.V.1, Mikhailov A.M.1
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Afiliações:
- Hypersonic Systems Research Institute
- Edição: Volume 54, Nº 3 (2016)
- Páginas: 397-402
- Seção: Heat and Mass Transfer and Physical Gasdynamics
- URL: https://journals.rcsi.science/0018-151X/article/view/156808
- DOI: https://doi.org/10.1134/S0018151X16030093
- ID: 156808
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Resumo
The problems of increasing the cooling capacity of hydrocarbon fuel by its thermochemical transformation in elements of thermal protection of a hypersonic flight vehicle and hydrogen production on board for providing stable burning in a scramjet are considered. A comparison of the chemical reactions of cracking and steam conversion of hydrocarbons, as regards the cooling capacity and amount of hydrogen in reaction products, is made. The process of steam conversion of methane in a thermochemical reactor and the factors influencing the conversion level of hydrocarbons are studied experimentally.
Sobre autores
A. Kuranov
Hypersonic Systems Research Institute
Email: mail@hypersonics.ru
Rússia, St. Petersburg, 196066
A. Korabel’nikov
Hypersonic Systems Research Institute
Email: mail@hypersonics.ru
Rússia, St. Petersburg, 196066
A. Mikhailov
Hypersonic Systems Research Institute
Autor responsável pela correspondência
Email: mail@hypersonics.ru
Rússia, St. Petersburg, 196066
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