¹Khorolskyi MS, Bigun SO. Performance of interface hoses for thermal conditioning system of "Cyclon-4" space rocket in extreme conditions. Space Science and Technology. 2021 ;27(4):11-20.

¹Degtyarev MA, ¹Akimov DV, ¹Bilous AS, ²Avramov KV. Thermal strength of retention compartment interacting with exhaust gas. Space Science and Technology. 2021 ;27(4):03-10.

¹Pylypenko OV, ²Degtyarev MA, ¹Nikolayev OD, ²Klimenko DV, ¹Dolgopolov SI, ¹Khoriak NV, ¹Bashliy ID, ²Silkin LA. Providing of POGO stability of the Cyclone-4M launch vehicle. Space Science and Technology. 2020 ;25(4):03-20.

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.