Development liquid rocket engine of small thrust with combustion chamber from carbon-ceramic composite material

Аuthors

Borovik I. N.^1*, Kazennov I. S.^1**, Lahin A. V.^2***, Bogachev E. A.², Timofeev A. N.²

1. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
2. Company «Composite», 4, Pioneerskaya str., Korolev, Moscow region, 141070, Russia

*e-mail: borovik.igor@mai.ru
**e-mail: heavigot@mail.ru
***e-mail: info@kompozit-mv.ru

Abstract

The technical paper about problem of development liquid rocket engine of small thrust with ceramic-composite combustion chamber. The review is presented of actual state of problem. The analysis of energy efficiency is presented for rocket engine of small thrust with ceramic-composite combustion chamber developing in MAI.

Keywords:

LRE of small thrust, combustion chamber, combustion chamber, carbon-ceramic composite material