The simulation of the orbital evolution of a passive high-orbit fragment with large surface area

dc.contributor.author	Bazyey, Oleksandr A.	en
dc.contributor.author	Базєй, Олександр Анатолійович	uk
dc.date.accessioned	2015-04-06T07:06:53Z
dc.date.available	2015-04-06T07:06:53Z
dc.date.issued	2014
dc.description.abstract	The numerical integration of the motion equations of a passive high-orbit fragment with large surface area was performed accounting for the main gravitational perturbations of the Earth, Moon and Sun, as well as the solar radiation pressure. Based on the numerical model of motion in the near-Earth space that accounts for only the most powerful perturbations, a new method for deorbiting artificial celestial bodies from high altitudes is suggested.	en
dc.identifier.citation	Odessa Astronomical Publications	en
dc.identifier.uri	https://dspace.onu.edu.ua/handle/123456789/6220
dc.language.iso	en
dc.publisher	Astroprint	en
dc.relation.ispartofseries	;V. 27, I. 2, P. 108-110.
dc.subject	numerical – celestial mechanics	en
dc.title	The simulation of the orbital evolution of a passive high-orbit fragment with large surface area	en
dc.type	Article	en

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