A study of boosters for recovery payload mass from geostationary orbit
Space technics and technology
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
AbstractIn 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.