Methane-oxygen liquid rocket engine of small thrust-development, design, tests and analysis of results

Аuthors

Kovateva Y. S.^*, Borovik I. N.^**, Hohlov A. N.^***, Kazennov I. S.^****

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: kovateva2005@rambler.ru
**e-mail: borovik.igor@mai.ru
***e-mail: kozlov202@mai.ru
****e-mail: heavigot@mail.ru

Abstract

The technical paper about problem of development oxygen/methane liquid rocket engine of small thrust. The review is presented of actual state of problem. The analysis computational and the experimental data received during firing tests at the Beijing University of Astronautics and Aeronautic (BUAA) is carried out.

Keywords:

LRE of small thrust, combustion chamber, oxygen-methane fuel.