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The influence of an external acoustic emission on wave processes arising in multiphase mechanical structures on board spacecraft 1Karachun VV, 1Kolosov VN. The influence of an external acoustic emission on wave processes arising in multiphase mechanical structures on board spacecraft. Kosm. nauka tehnol. 1996 ;2(1):68–72.
Improving the efficiency of meteorological rockets with the use of hybrid engines 1Oriekhov KM. Improving the efficiency of meteorological rockets with the use of hybrid engines. Kosm. nauka tehnol. 2016 ;22(2):52-59.
Problems of development of controlling liquid jet system, which is powered from lines of a booster of the launch vehicle upper stage 1Timoshenko VI, 2Knyshenko Yu.V, 3Durachenko VM, 4Anishchenko VM. Problems of development of controlling liquid jet system, which is powered from lines of a booster of the launch vehicle upper stage. Kosm. nauka tehnol. 2016 ;22(1):20-35.
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.
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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.