Conversion of hydrocarbon fuel in elements of thermal protection of a hypersonic flight vehicle


Citar

Texto integral

Acesso aberto Acesso aberto
Acesso é fechado Acesso está concedido
Acesso é fechado Somente assinantes

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

Arquivos suplementares

Arquivos suplementares
Ação
1. JATS XML

Declaração de direitos autorais © Pleiades Publishing, Ltd., 2016