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.

¹Bobukh KA, ¹Bobukh TA, ¹Bobukh LV. Conception of energy and elemental change of substance state. Kosm. nauka tehnol. 2003 ;9(Supplement1):093-097.

¹Lysenko AS. Development of rated-analytical method for registration of stress relaxation effect on functionality of units of flight vehicle engine. Kosm. nauka tehnol. 2003 ;9(Supplement1):088-092.

¹Chaplygina Yu.S, ¹Stovpcheriko AP, ²Tarasov AL. The study of mechanical and corrosion properties of lead strip for chemical sources of electric power. Kosm. nauka tehnol. 2003 ;9(Supplement1):084-088.

¹Ambrozhevich AV, ¹Potapenko AA, ¹Lar'kov SN, ¹Yashin SA, ¹Simbirskii VL, ¹Belyakov KV. Air-breathing engines for unmanned flight micro-vehicles. Kosm. nauka tehnol. 2003 ;9(Supplement1):078-084.

¹Vorotintsev EV, ²Sokol GI. Mathematical modelling the propagation of shock waves from explosion in ground. Kosm. nauka tehnol. 2003 ;9(Supplement1):065-067.