Space Energy, Power and Propulsion

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

Ensuring re-launch in flight of the steering engine, made according to the scheme with afterburning of generator gas