Space Energy, Power and Propulsion

The approach to numerical simulation of the spatial movement of fluid with forming free gas inclusions in propellant tank at space flight conditions

Study of the temperature and force effects of supersonic jets of the space rockets on the gas duct of the launch complex during the water supply system operation

Problems and ways of their solutions in the development of a lowthrust liquid jet engine for a stage 3 liquid jet system of «Cyclone-4» launch vehicle

Mathematical modeling of dynamic processes in feeding system of space stage main engine of launch vehicle at active and passive flight