Zobrazeno 1 - 10
of 40
pro vyhledávání: '"Golubek, A."'
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2021, Vol. 94, Issue 4, pp. 505-514.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-04-2021-0100
Publikováno v:
Eastern-European Journal of Enterprise Technologies; 2024, Vol. 129 Issue 7, p63-72, 10p
Autor:
A.V. Golubek, G.V. Farafonov
Publikováno v:
Journal of Rocket-Space Technology. 30:81-89
Робота присвячена розробці методу планування включення електрореактивної двигунної установки для забезпечення стабілізації висот
Publikováno v:
Eastern-European Journal of Enterprise Technologies. 5:6-16
This paper reports a study into the influence exerted by the thermal flows of space environment on the deformation of the shell of a space inflatable platform with a payload. The mathematical model of the effect of temperature fluctuations on the mas
Autor:
A.V. Golubek
Publikováno v:
Proceedings of Higher Educational Institutions. Маchine Building. :101-111
The article proposes the development of a method for the combined deorbiting large space debris objects from low Earth orbits, performed using an electric propulsion engine and an aerodynamic sailing device. Simulation modeling of the combined deorbi
Publikováno v:
Journal of Rocket-Space Technology. 29:179-189
Для очищення верхнього сегменту низьких навколоземних орбіт з висотою 1400-2000 км запропоновано використання комбінованого методу відвед
Publikováno v:
Aircraft Engineering and Aerospace Technology. 94:505-514
Purpose Leading developers and providers in the modern space launch market note a splash in the development of ultralight launch vehicle (LV), driven by the growing demand for small satellites for large constellations in low Earth orbits. One of the
Publikováno v:
CEAS Space Journal; Jul2023, Vol. 15 Issue 4, p613-625, 13p
Autor:
A.V. Golubek, N.M. Dron
Publikováno v:
Science and innovation. 16:46-55
Introduction. A constant increase in the amount of space debris already constitutes a significant threat to satellites in nearEarth orbits, starting with the trajectory of their launch vehicle injection. Problem Statement. Design and development of v