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This article is cited in 5 scientific papers (total in 5 papers)
Heat and Mass Transfer and Physical Gasdynamics
Conversion of hydrocarbon fuel in elements of thermal protection of a hypersonic flight vehicle
A. L. Kuranov, A. V. Korabel'nikov, A. M. Mikhailov Science and Research Organization for Hypersonic Systems, Saint-Petersburg
Abstract:
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.
Received: 22.07.2014 Accepted: 05.11.2014
Citation:
A. L. Kuranov, A. V. Korabel'nikov, A. M. Mikhailov, “Conversion of hydrocarbon fuel in elements of thermal protection of a hypersonic flight vehicle”, TVT, 54:3 (2016), 423–429; High Temperature, 54:3 (2016), 397–402
Linking options:
https://www.mathnet.ru/eng/tvt1401 https://www.mathnet.ru/eng/tvt/v54/i3/p423
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Abstract page: | 307 | Full-text PDF : | 280 | References: | 60 | First page: | 1 |
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