Search
] . About the classification of launch equipment of the space launch systems for the strength standards justification. Kosm. nauka tehnol. 2016 ;22(1):03-14.
. Accuracy assessment of the temperature of artificial and natural Earth’s surfaces determining by infrared satellite imagery. Kosm. nauka tehnol. 2016 ;22(4):19-28.
. Effiecency criterion for selection of design parameters of aerospace system. Kosm. nauka tehnol. 2016 ;22(2):48-51.
. Evaluation of the use of polyurethane in a solid rocket fuel for a single stage launch vehicle — carrier of an unmanned spacecraft orbiter for orbital and suborbital flights. Kosm. nauka tehnol. 2016 ;22(1):36-51.
. Evaluation of the use of polyurethane in a solid rocket fuel for a single stage launch vehicle — carrier of an unmanned spacecraft orbiter for orbital and suborbital flights. Kosm. nauka tehnol. 2016 ;22(1):36-51.
. Foreword on occasion of the 100th issue of the "Space Science and Technology":by Editor-in-Chief. Kosm. nauka tehnol. 2016 ;22(3):03-03.
. Influence of magnetic field on the properties of paraffin based fuel for hybrid rocket engines. Kosm. nauka tehnol. 2016 ;22(3):16-24.
. ORBIT CHANGES UNDER THE SMALL CONSTANT DECELERATION. Kosm. nauka tehnol. 2016 ;22(6):20-25.
. Achieving spacecraft rapid rotation using minimally redundant coplanar gyrodyne system. Kosm. nauka tehnol. 2015 ;21(5):48–56.
. The advanced liquid rocket engine line of SDO “Yuzhnoye” for the creation of new families of launch vehicles. Kosm. nauka tehnol. 2015 ;21(5):28–35.