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

1Durachenko VM, 1Shpak AV, 1Kolesnychenko SA, 1Aheyeva LI, 1Dolinkevich AS, 1Unchur KO. 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. Space Science and Technology. 2020 ;26(1):18-29.

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

1Pylypenko OV, 1Nikolayev OD, 2Bashliy ІD, 1Dolgopolov SI. Mathematical modeling of dynamic processes in feeding system of space stage main engine of launch vehicle at active and passive flight. Space Science and Technology. 2020 ;26(1):03-17.

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

1Prokopenko Yu.A, 1Strelchenko EV, 1Pisarenko VYu., 1Sinitsyn DYu., 1Troyak AB, 1Shementov AN. Ensuring re-launch in flight of the steering engine, made according to the scheme with afterburning of generator gas. Kosm. nauka tehnol. 2004 ;10(Supplement1):034-038.

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

1Mahdin EK, 1Dmytrenko YS, 1Tolochyants HE, 1Mikhaylov MS, 1Filippov VV, 1Ohlikh VV. 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. Space Science and Technology. 2019 ;25(6):33-38.

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