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.

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.

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.

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.

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.

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.

¹Marchan RA. Ignition system for combustion chambers operating on air+kerosene propellants. Kosm. nauka tehnol. 2003 ;9(Supplement1):128-132.

¹Onishchenko SM. Stand for the check up on the operation of opening mechanisms of solar batteries. Kosm. nauka tehnol. 2003 ;9(Supplement1):109-111.

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.

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