You are here

Space Energy, Power and Propulsion

Mathematical modeling of the processes of air gas thermodynamics of the supersonic aircraft with a ramjet

¹Timoshenko VI, ¹Galinskiy VP. Mathematical modeling of the processes of air gas thermodynamics of the supersonic aircraft with a ramjet. Space Science and Technology. 2020 ;26(2):03-18.

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, ¹Nikolaev AD, ¹Bashliy 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.

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.

Theoretical and experimental aspects of ultrasonic restoration of alkaline accumulators

Bezruchko K, Vasilenko A, Davidov A, Kharchenko A. Theoretical and experimental aspects of ultrasonic restoration of alkaline accumulators. Kosm. nauka tehnol. 2003 ;9(Supplement1):147-149.

The fitting of parameters of the hyperacoustic entering device and afterburning chamber of the rocket-based-combined-cycle engine

¹Katrenko MA, Gorbenko GA. The fitting of parameters of the hyperacoustic entering device and afterburning chamber of the rocket-based-combined-cycle engine. Kosm. nauka tehnol. 2003 ;9(Supplement1):139-142.

Ignition system for combustion chambers operating on air+kerosene propellants

Marchan RA. Ignition system for combustion chambers operating on air+kerosene propellants. Kosm. nauka tehnol. 2003 ;9(Supplement1):128-132.

Stand for the check up on the operation of opening mechanisms of solar batteries

Onishchenko SM. Stand for the check up on the operation of opening mechanisms of solar batteries. Kosm. nauka tehnol. 2003 ;9(Supplement1):109-111.

Simulation of propellant component utilization in the test bench environment by the gas injection into the engine feed lines

Prokopenko YA, Strel'chenko EV. Simulation of propellant component utilization in the test bench environment by the gas injection into the engine feed lines. Kosm. nauka tehnol. 2003 ;9(Supplement1):105-108.

The design of the power supply system for spacecraft of the microsatelute type

¹Alikperov RR, Guhin SV, Gorovyi AV. The design of the power supply system for spacecraft of the microsatelute type. Kosm. nauka tehnol. 2003 ;9(Supplement1):101-105.

Pages