Space Energy, Power and Propulsion
Determination of a force transmitted by a plume of an ion thruster to an orbital object
Determination of a force transmitted by a plume of an ion thruster to an orbital object. Kosm. nauka tehnol. 2016 ;22(1):52-63.
. Radiation susceptibility of supercapacitors and prospects for their space applications
Radiation susceptibility of supercapacitors and prospects for their space applications. Kosm. nauka tehnol. 2013 ;19(3):47–60.
Kerosene fuel tank super-cold pressurization system parameters mathematical modeling
Kerosene fuel tank super-cold pressurization system parameters mathematical modeling. Kosm. nauka tehnol. 2015 ;21(5):43–47.
. Pneumopump feed system of propellant components in liquid rocket engines and power installations
Pneumopump feed system of propellant components in liquid rocket engines and power installations. Kosm. nauka tehnol. 2015 ;21(5):36–42.
. The advanced liquid rocket engine line of SDO “Yuzhnoye” for the creation of new families of launch vehicles
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.
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