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Space Energy, Power and Propulsion

Increasing of reliability of large demension bellow in launch vehicle fuel system

¹Olovarenko Yu.V. 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

¹Nakashidze LV, ²Zarivnyak GL, ²Mitrokhov SA. 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

¹Zhivotov AYu. 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

¹Zabarko DA, ¹Kotenev VP. 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

¹Redchits D, ¹Prykhodko A. 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

¹Maksymenko TA, ¹Loyan AV, ¹Koshelev NN. 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

¹Shevchenko BA, ¹Nazarenko EP, ¹Ivanov ОМ. 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

¹Bulanenko VYe., ¹Avdeev VV. 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

¹Zolotko OE, ¹Zolotko OV, ¹Moroz Yu.I, ¹Sosnovska OV. The burned gas with external environment in the pulse detonation engine chamber turbulent mixing model. Space Sci. & Technol. 2018 ;24(6):16-23.

Prediction of gear wear for the estimation of solar array drive dynamic behavior

¹Shatikhin VE, ²Semenov LP, ³Khoroshylov VS, ³Popel' VM, ⁴Kostenko GA. Prediction of gear wear for the estimation of solar array drive dynamic behavior. Kosm. nauka tehnol. 2006 ;12(4):033-037.

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