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.
Numerical simulation of efflux of a supersonic multicomponent chemical reacting rocket engine jet 1Timoshenko VI, 2Deshko HYe. Numerical simulation of efflux of a supersonic multicomponent chemical reacting rocket engine jet. Kosm. nauka tehnol. 2017 ;23(6):03-11.
Method of determination of types and parameters of the electric energy storage system during its operation in autonomous power supply system of mobile space launch complex 1Zemlyany KM, 1Reva VS, 1Frolov VP, 2Bezruchko KV. Method of determination of types and parameters of the electric energy storage system during its operation in autonomous power supply system of mobile space launch complex. Space Science and Technology. 2017 ;23(5):25-32.
Mathematical modelling of introballistic characteristic of solid rocket engine with power-on emergency shutdown system 1Lytvynenko VYe., 1Kalnysh RV, 1Popov VA. Mathematical modelling of introballistic characteristic of solid rocket engine with power-on emergency shutdown system. Space Science and Technology. 2017 ;23(5):21-24.
Simulation of motion of ions in the channel of a stationary plasma thruster 1Petrenko OM, 2Bucharskyi VL. Simulation of motion of ions in the channel of a stationary plasma thruster. Space Science and Technology. 2017 ;23(5):14-20.
Pequliarities of mathematical modeling of low-frequency dynamics of the staged liquid rocket sustainer engines at its startup 1Pylypenko OV, 2Prokopchuk AA, 1Dolgopolov SI, 2Pisarenko VYu., 2Kovalenko VN, 1Nikolaev AD, 3Khoryak NV. Pequliarities of mathematical modeling of low-frequency dynamics of the staged liquid rocket sustainer engines at its startup. Space Science and Technology. 2017 ;23(5):03-13.
New method for the transformation of solar radiation energy into electric power for energy feeding of the space vehicles 1Ludanov KI. New method for the transformation of solar radiation energy into electric power for energy feeding of the space vehicles. Kosm. nauka tehnol. 2007 ;13(6):031-038.