Particularity of investigation of reliability for liquid rocket engine during its projecting
. Particularity of investigation of reliability for liquid rocket engine during its projecting. Kosm. nauka tehnol. 2001 ;7(Supplement1):047-050.
Space Energy, Power and Propulsion
Increasing of reliability of large demension bellow in launch vehicle fuel system
. Increasing of reliability of large demension bellow in launch vehicle fuel system. Kosm. nauka tehnol. 2001 ;7(Supplement1):040-043.
On use of optimum operation mode of solar cell
. On use of optimum operation mode of solar cell. Kosm. nauka tehnol. 2001 ;7(Supplement1):038-039.
Liquid balancing device for static balancing under constant final liquid flow rate. balancing accuracy
Liquid balancing device for static balancing under constant final liquid flow rate. balancing accuracy. Kosm. nauka tehnol. 2001 ;7(Supplement1):033-037.
Numerical investigation of viscous chemically reacting gas flows near blunt-nosed bodies in the framework of Navier–Stokes equations
. Numerical investigation of viscous chemically reacting gas flows near blunt-nosed bodies in the framework of Navier–Stokes equations. Kosm. nauka tehnol. 2005 ;11(Supplement1):036-042.
The numerical decision of the connected problem of dynamics and aerodynamics of wind turbine rotor
. The numerical decision of the connected problem of dynamics and aerodynamics of wind turbine rotor. Kosm. nauka tehnol. 2005 ;11(Supplement1):027-035.
Probe diagnostics of low-power stationary plasma thruster plume
. Probe diagnostics of low-power stationary plasma thruster plume. Kosm. nauka tehnol. 2005 ;11(Supplement1):024-027.
Effect of ІІ stage propulsion system shut-down transients on launch vehicle performance capability
. Effect of ІІ stage propulsion system shut-down transients on launch vehicle performance capability. Kosm. nauka tehnol. 2005 ;11(Supplement1):021-023.
Influence of thrust/weight ratio of a space vehicle on a transition duration from a near-earth to a near-lunar orbit
. Influence of thrust/weight ratio of a space vehicle on a transition duration from a near-earth to a near-lunar orbit. Kosm. nauka tehnol. 2005 ;11(Supplement1):018-020.
The burned gas with external environment in the pulse detonation engine chamber turbulent mixing model
. The burned gas with external environment in the pulse detonation engine chamber turbulent mixing model. Space Sci. & Technol. 2018 ;24(6):16-23.