350 rub
Journal Science Intensive Technologies №8 for 2016 г.
Article in number:
Offering for creating low orbit multi-satellite communicato in system subject to available group launch vehicle on near-earth orbit
Keywords: satellite communications spacecrafts low circular orbit launch vehicle
Authors:
A.V. Kyzovnikov - Ph. D. (Eng.), Associate Professor, Reshetnev Siberian State Aerospace University (Krasnoyarsk); Head of Department, JSC Academician M.F. Reshetnev «ISS» (Zheleznogorsk). E-mail: ujub@list.ru V.E. Kosenko - Dr. Sc. (Eng.), Professor, First Deputy General Director and General Designer, JSC Academician M.F. Reshetnev «ISS» (Zheleznogorsk) V.V. Golovkov - Post-graduate Student, Reshetnev Siberian State Aerospace University (Krasnoyarsk); Engineer, JSC Academician M.F. Reshetnev «ISS» (Zheleznogorsk) S.N. Leonov - Design Engineer, JSC Academician M.F. Reshetnev «ISS» (Zheleznogorsk) I.I. Zimin - Post-graduate Student, Reshetnev Siberian State Aerospace University (Krasnoyarsk); Design Engineer, JSC Academician M.F. Reshetnev «ISS» (Zheleznogorsk)
Abstract:
The article describes the main characteristics of the orbital grouping promising foreign satellite communication systems OneWeb. According to the results of computer simulation it was proposed two options for building the orbital group of spacecraft in a low circular orbit for sustainable global coverage over the Earth. A comparison of current and future launch vehicles of domestic production, which can be used as a means of small class spacecraft into a low circular orbit in terms of optimizing the value creation system. In addition, it compares the cost of the deployment of the national system of satellite communication with foreign counterparts.
Pages: 25-29
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