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. Research of supersonic flow in shortened nozzles of rocket engines with a bell-shaped tip. Space Science and Technology. 2024 ;30(1):03-13.
. The influence of the entrance angle to the bell-shaped tip of a shortened round supersonic nozzle of a rocket engine on its impulse characteristics. Space Science and Technology. 2024 ;30(3):53-60.
. Investigation of heat exchange for mobile steam generators with a purpose of utilization of power plants. Kosm. nauka tehnol. 2001 ;7(Supplement1):050-053.
. Reasons determination of liquid rocket engine damage situations using engine experiment data. Kosm. nauka tehnol. 2002 ;8(Supplement1):040-045.
. Methods of allowing for earth's atmosphere influence in space geodesy and navigation. Kosm. nauka tehnol. 2001 ;7(4):163–168.
. 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.
. 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.
. The advanced liquid rocket engine line of SDO “Yuzhnoye” for the creation of new families of launch vehicles. Kosm. nauka tehnol. 2015 ;21(5):28–35.
. The limit accuracy of laser ranging of Earth artificial satellites. Kosm. nauka tehnol. 1996 ;2(2):70–81.