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Space Energy, Power and Propulsion

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.

Influence of ionization and acceleration chamber geometry on the characteristics of a stationary plasma engine

¹Balashov VN. Influence of ionization and acceleration chamber geometry on the characteristics of a stationary plasma engine. Kosm. nauka tehnol. 2004 ;10(Supplement1):030-033.

Experimental research of the power characteristics of solar cells of various types at natural illumination

¹Nakashidze LV, ¹Degtyarova NV, ¹Zarivnyak GL, ²Mitrokhov SA. Experimental research of the power characteristics of solar cells of various types at natural illumination. Kosm. nauka tehnol. 2004 ;10(Supplement1):016-018.

Methods of measurement of charges of liquids are considered at dynamic tests of hydraulic automatic devices

¹Korbanyuk SR. Methods of measurement of charges of liquids are considered at dynamic tests of hydraulic automatic devices. Kosm. nauka tehnol. 2004 ;10(Supplement1):013-015.

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

¹Bezruchko KV, ²Vasilenko A, ²Davidov A, ²Kharchenko 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, ¹Gorbenko 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

¹Marchan 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

¹Onishchenko 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

¹Prokopenko Yu.A, ¹Strelchenko 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.

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