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

Autor: D. M. Yagodnikov, K. O. Chertkov, Yu. V. Antonov, A. Novikov

Publikováno v: Aèrokosmičeskij Naučnyj Žurnal, Vol 1, Iss 05, Pp 12-25 (2015)
Aèrokosmičeskij Naučnyj Žurnal, Vol 1, Iss 05, Pp 12-25 (2016)

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 an

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::a2b3e7b72a362e1eef0f4322be648317
http://aerospace.elpub.ru/jour/article/view/25