Providing of POGO stability of the Cyclone-4M launch vehicle 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.
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 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.
To equistability problem of the reinforced shell structure under combined loading 1Degtyarenko PG, 2Grishchak VZ, 3Grishchak DD, 2Dyachenko NM. To equistability problem of the reinforced shell structure under combined loading. Space Science and Technology. 2019 ;25(6):03-14.
Inclusion of the economic factor for making a decision in the pre-launch procedure of a launcher 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.
Evaluation of hazard for linear objects in case of launch vehicle failure in flight phase 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.
Optimization of design parameters of the main composite fairing of the launch vehicle under simultaneous force and thermal loading 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.
Mathematical model of the rocket motion relative to a mobile launcher 1Degtyareva ЕА, 1Novykov OV. Mathematical model of the rocket motion relative to a mobile launcher. Space Sci. & Technol. 2019 ;25(3):03-15.
Development of diagnosing conception of source technical availability of automated elements of pneumohydraulic launch vehicle systems 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.
Space industry development in organization scheme of the Ukrainian national economy 1Dzhur OE. Space industry development in organization scheme of the Ukrainian national economy. Kosm. nauka tehnol. 2002 ;8(Supplement1):016-020.
Study of environment parameters that determine ilv «Zenit-3SL» loading during standing before launch 1Arlekinova ОЕ. Study of environment parameters that determine ilv «Zenit-3SL» loading during standing before launch. Kosm. nauka tehnol. 2002 ;8(Supplement1):009-011.