The plume-flows structure of spacecraft thrusters 1Shuvalov VA, 2Kochubei GS, 2Lazuchenkov DN. The plume-flows structure of spacecraft thrusters. Kosm. nauka tehnol. 2003 ;9(4):017-025.
Degradation of parameters of solar cells under the influence of open space factors 1Zhenyu Hu, 2Abraimov VV, 1Shiyu He., 1Dezhuang Y, 3Rassamakin BM. Degradation of parameters of solar cells under the influence of open space factors. Kosm. nauka tehnol. 2003 ;9(1):081-091.
Small Experimental Electrodynamic Space Tether System. Electrical model 1Pirozhenko AV, 2Mischenko AV. Small Experimental Electrodynamic Space Tether System. Electrical model. Space Science and Technology. 2018 ;24(3):03-09.
Project of a small experimental electrodynamic space tether system 1Pirozhenko AV, 1Maslova AI, 2Mischenko AV, 2Khramov DA, 2Voloshenjuk OL. Project of a small experimental electrodynamic space tether system. Space Science and Technology. 2018 ;24(2):03-11.
Analysis of vibroacoustic condition of rocket engines by radar techniques 1Ermilov Yu.V. Analysis of vibroacoustic condition of rocket engines by radar techniques. Kosm. nauka tehnol. 2002 ;8(5-6):107-111.
Feasibility of the ultrasound checking of the first-stage engine of the Zenith rocket carrier. 2. Results of the ultrasound diagnostics of the engine defectiveness 1Bezymyannyi Yu.G, 1Borovik VG, 2Galas' MI, 1Trefilov VI, 1Frolov GA. Feasibility of the ultrasound checking of the first-stage engine of the Zenith rocket carrier. 2. Results of the ultrasound diagnostics of the engine defectiveness. Kosm. nauka tehnol. 2002 ;8(1):032-036.
Probabilistic estimation of electric energy supply for spacecraft 1Belov DG. Probabilistic estimation of electric energy supply for spacecraft. Kosm. nauka tehnol. 2002 ;8(4):037-042.
Degradation of the electric power of solar arrays under the influence of the near-satellite environment in geostationary orbits 1Shuvalov VA, 2Kochubey GS, 2Priimak AI, 2Reznichenko NP. Degradation of the electric power of solar arrays under the influence of the near-satellite environment in geostationary orbits. Kosm. nauka tehnol. 2002 ;8(4):025-036.
Methane, kerosene and hydrogen comparative as a rocket fuel for launch vehicle pneumohydraulic supply system development 1Mykhalchyshyn RV, 1Brezgin MS, 1Lomskyi DA. Methane, kerosene and hydrogen comparative as a rocket fuel for launch vehicle pneumohydraulic supply system development. Kosm. nauka tehnol. 2018 ;24(2):12-17.
Influence of cutouts on strength of cylindrical compartments of launch vehicles at inelastic deformation of material 1Hudramovich VS, 2Klymenko DV, 3Hart EL. Influence of cutouts on strength of cylindrical compartments of launch vehicles at inelastic deformation of material. Kosm. nauka tehnol. 2017 ;23(6):12-20.