Engines for advanced launch-vehicles of heavy and super-heavy classes

Paper number

IAC-14,C4,P,27,x21458

Author

Mr. Vladimir Sudakov, JSC NPO Energomash, Russian Federation

Coauthor

Dr. Vladimir K. Chvanov, NPO Energomash, Russian Federation

Coauthor

Dr. Vadim Semenov, JSC NPO Energomash, Russian Federation

Coauthor

Mr. Vladimir Gusev, JSC NPO Energomash, Russian Federation

Coauthor

Mr. Dmitry Pushkarev, JSC NPO Energomash, Russian Federation

Coauthor

Dr. Levochkin Petr, NPO Energomash, Russian Federation

Year

2014

Abstract

Family of unified oxygen-kerosene rocket engines with unique power and performance characteristics has created at JSC «NPO Energomash». Such family allows to carry out work on its modernization in relation to the use in launch-vehicles of absolutely any class, satisfying the needs of any world's leading designers of launch-vehicles. 
	LPRE of this family with a wide range of throttling (from 105% to 30% of nominal mode) provide thrust in the range from 0.58 up to 9.81 MN. Orientation for such LPRE provides creation of new LV of any class with a minimum of risk and expanses.
	Succession of design, unification of technical solutions, materials, production processes and high operating performance allows to improve the engines in terms of expansion of the family, minimizing the expanses and providing high quality and reliability, that allows in the shortest terms and with high quality to conduct, particularly, the modernization of engines for advanced launch-vehicles.
	NPO Energomash is working on creation of new powerful reusable LPRE for advanced reusable launch-vehicles.

Abstract document

IAC-14,C4,P,27,x21458.brief.pdf

Manuscript document

(absent)