Numerical Study of the Working Process in the Reducing Gas Generator of the Upper Stage Oxygen - Methane Engine

<p>This article deals with the problems of creating a reducing gas generator of the liquid rocket engine (LRE) of upper stage using advanced fuel components, namely oxygen + liquid natural gas. Relevance of the work is justified by the need to create and develop of environmentally friendly mis...

Full description

Bibliographic Details
Main Authors: D. M. Yagodnikov, K. O. Chertkov, Yu. V. Antonov, A. Novikov
Format: Article
Language:Russian
Published: MGTU im. N.È. Baumana 2015-01-01
Series:Aèrokosmičeskij Naučnyj Žurnal
Subjects:
Online Access:http://aerospace.elpub.ru:80/jour/article/view/25