SMALL EXPERIMENTAL ELECTRODYNAMIC SPACE TETHER SYSTEM. ELECTRICAL MODEL
. SMALL EXPERIMENTAL ELECTRODYNAMIC SPACE TETHER SYSTEM. ELECTRICAL MODEL. Space Science and Technology. 2018 ;24(3):03-10.
Space Energy, Power and Propulsion
Project of a small experimental electrodynamic space tether system
. 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
. 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
. 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
. 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
. 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
. 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
. 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
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
. 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.