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Redchits D, Prykhodko A. The numerical decision of the connected problem of dynamics and aerodynamics of wind turbine rotor. Kosm. nauka tehnol. 2005 ;11(Supplement1):027-035.

Maksymenko TA, Loyan AV, Koshelev NN. Probe diagnostics of low-power stationary plasma thruster plume. Kosm. nauka tehnol. 2005 ;11(Supplement1):024-027.

Shevchenko BA, Nazarenko EP, Ivanov ОМ. Effect of ІІ stage propulsion system shut-down transients on launch vehicle performance capability. Kosm. nauka tehnol. 2005 ;11(Supplement1):021-023.

Bulanenko VY, 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.

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

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

¹Pokhyl Yu.A, ²Gavrylov RV, ¹Yakovenko LF, ¹Aleksenko EN, ¹Lototskaya VA, ³Xiaoyan Wang, ³Shiyu He., ⁴Tarasov GV, ⁵Rassamakin BM. Mechanical characteristics of major components of solar arrays. Kosm. nauka tehnol. 2006 ;12(4):024-032.

¹Belov DG. Electric power supply of spacecraft fail-safety under solar array pointing failure. Kosm. nauka tehnol. 2006 ;12(4):020-023.

¹Yemets VV. Experimental study of rocket engine model with gaseous polyethylene fuel. Kosm. nauka tehnol. 2006 ;12(2-3):103-107.