¹Gladkyi EG. Determination of the collective risk in a case of a launch vehicle «Cyclon-4M» crash during the flight phase using polygon images to represent populated areas. Space Science and Technology. 2020 ;26(3):32-41.

¹Degtyarenko PG, ²Grishchak VZ, ³Grishchak DD, ⁴Dyachenko NM. To equistability problem of the reinforced shell structure under combined loading. Space Science and Technology. 2019 ;25(6):03-14.

¹Zhuk S, ²Fediakin AI, Agarkow AV. Inclusion of the economic factor for making a decision in the pre-launch procedure of a launcher. Kosm. nauka tehnol. 2003 ;9(Supplement1):074-077.

¹Hladkii EH. Evaluation of hazard for linear objects in case of launch vehicle failure in flight phase. Space Science and Technology. 2019 ;25(4):22-28.

¹Kondratiev AV, ²Kovalenko VO. Optimization of design parameters of the main composite fairing of the launch vehicle under simultaneous force and thermal loading. Space Science and Technology. 2019 ;25(4):03-21.

¹Degtyareva ЕА, ¹Novykov OV. Mathematical model of the rocket motion relative to a mobile launcher. Space Sci. & Technol. 2019 ;25(3):03-15.

¹Ponomaryov AN, ¹Sichevoy AV. Development of diagnosing conception of source technical availability of automated elements of pneumohydraulic launch vehicle systems. Kosm. nauka tehnol. 2002 ;8(Supplement1):036-040.

¹Dzhur OE. Space industry development in organization scheme of the Ukrainian national economy. Kosm. nauka tehnol. 2002 ;8(Supplement1):016-020.

¹Arlekinova ОЕ. Study of environment parameters that determine ilv «Zenit-3SL» loading during standing before launch. Kosm. nauka tehnol. 2002 ;8(Supplement1):009-011.

¹Lager TL. Accuracy analysis of determination of angular displacements on the basis of measurements of linear displacements. Kosm. nauka tehnol. 2001 ;7(Supplement1):060-063.