Substantiation of rational flight multiplication factor of using rocket engines and glider in the system's perspective reusable launch vehicles of payload in orbits

Аuthors

Sadchikov I. I.^*, Chulcov S. A.

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

*e-mail: k501@mai.ru

Abstract

This article presents the estimation of rational flight multiplication factor of using propulsion system and glider in the system oj perspective reusable rocket on criterion general costs and production output in view of safety launch vehicle.

Keywords:

propulsion system, launch vehicle, payload, launching site, glider