Space Energy, Power and Propulsion

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

Optimization of the design of pulse solid-propellant rocket engines with metal bodies by their association in the monoblock compartment made of high-strength plastic

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