A study of boosters for recovery payload mass from geostationary orbit

Space technics and technology


Shcherbakova E. A.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

e-mail: scherbakova@oboronprom.ru


In activity, the research of the project of a space vehicle is carried out on the basis of present boosters with a problem of returning from geostationary orbit (GSO) of the refused artificial satellites of the Earth with the preliminary analysis of the mass-power characteristics of possible versions of operation. Three versions of the possible scripts of operation of returning of a payload mass are considered. By results of the conducted calculations, the conclusions with the instruction of the most expedient version of returning of a payload mass are done.


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