Thrust enhancing for nozzle assembly of a liquid-propellant rocket engine within dense atmosphere layers using atmospheric air

Аuthors

Talalayev A. A.

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

Abstract

An improvement of a structure is suggested for automatic-adjusted nozzle assembly of a liquid-propellant rocket engine intended as a cruise one for the first stage of a launch vehicle. The improvement allows to enhance operational properties of the engine within dense atmosphere layers using atmospheric air, i.e. during initial path segments.