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Space Energy, Power and Propulsion

Evaluation of the use of polyurethane in a solid rocket fuel for a single stage launch vehicle — carrier of an unmanned spacecraft orbiter for orbital and suborbital flights

¹Levenko AS, ²Prysiazhnyi VI, ³Pauk OL, ⁴Drozdenko AS. Evaluation of the use of polyurethane in a solid rocket fuel for a single stage launch vehicle — carrier of an unmanned spacecraft orbiter for orbital and suborbital flights. Kosm. nauka tehnol. 2016 ;22(1):36-51.

Determination of a force transmitted by a plume of an ion thruster to an orbital object

¹Alpatov AP, ²Zakrzhevskii AE, ³Merino M, ⁴Fokov AA, ⁵Khoroshylov SV, ³Cichocki F. 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

¹Klymenko Yu.O, ¹Semeniv OV, Bezpalova AV, ¹Prutsko Yu.V, ²Maletin Yu.A, ²Stryzhakova NG, ²Zelinskyi SA, ²Tychyna SO, ²Drobnyi DM, ³Neymash VB, et al. 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

¹Mitikov Yu.А. 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

¹Konokh VI, ¹Gordiets IM. 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

¹Prokopchuk AA, ¹Shulga VА. 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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