Selecting the conditions of nanosatellite separation from the upper stage of the  arrier-rocket "Soyuz" in undirected flight

Аваряскин Д. П.; D. P. Avaryaskin; Белоконов И. В.; I. V. Belokonov; Тимбай И. А.; I. A. Timbay; Лагно О. Г.; O. G. Lagno

doi:10.18287/1998-6629-2013-0-4(42)-9-18

Selecting the conditions of nanosatellite separation from the upper stage of the arrier-rocket "Soyuz" in undirected flight

Authors: Avaryaskin D.P.¹, Belokonov I.V.¹, Timbay I.A.¹, Lagno O.G.²
Affiliations:
1. Samara State Aerospace University
2. Space Rocket Center “TsSKB-Progress”, Samara
Issue: Vol 12, No 4 (2013)
Pages: 9-18
Section: ISSUE WITHOUT SECTION
URL: https://journals.ssau.ru/vestnik/article/view/18
DOI: https://doi.org/10.18287/1998-6629-2013-0-4(42)-9-18
ID: 18

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Abstract

The paper presents a stochastic investigation that made it possible to develop a methodology for selecting the control parameters of nanosatellite separation (velocity and time of the separation) excluding the possibility of a collision in subsequent motion. Numerical results are given for the case of launching a nanosatellite from the upper stage of “Soyuz” carrier rocket.