Algorithm of common designing of the reusable booster for geostationary operations

Aerospace propulsion engineering


Аuthors

Shcherbakova E. A.

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

e-mail: scherbakova@oboronprom.ru

Abstract

The problem of common designing of the reusable booster for fulfilment of geostationary operations is put. On the basis of present boosters for clearing of geostationary orbit (GSO) from disabled artificial satellites of the Earth is regarded an issue of designing of a special flight vehicle. In activity the preliminary parametric analysis by criteria of an economic efficiency of operation, in result is carried conducted which is concluded a ratio of main specifications for an economically expedient projected system.


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