| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1716154 | Acta Astronautica | 2009 | 7 Pages |
Abstract
Some problems of methane-containing hydrocarbon fuel combustion are discussed. It seems that reduction of methane burnout zone length is one from main problems of designing new type engine. It is very important at the creation of combustion chambers of a rocket-ramjet engine for prospective space shuttle launch vehicles.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Valeriy I. Timoshenko, Igor S. Belotserkovets, Vjacheslav P. Gusinin,