Advanced astrophysical system segment evolution and stability

Аuthors

Kovkov G. V.¹, Malyshev V. V.^2*, Fedorov A. V.^2**

1. Central Research Institute of Machine Building, 4, Pionerskaya st., Korolev, Moscow region, 141070, Russia
2. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: veniaminmalyshev@mail.ru
**e-mail: alexanderf@mail.ru

Abstract

Ballistic layout for advanced astrophysical space system is under consideration. Spatially scattered spacecraft orbits dynamics is analyzed. An approach to maximize an arm of a radio interferometer at the expense of a high apogee orbit disturbance is suggested. Numerical simulation results are given.

Keywords:

astrophysical complex, high apogee orbit, high circular orbit, stability, evolution, space segment