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Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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Search by keyword: "constellation of satellites"


Mathematical model of a maneuvering nanosatellite with a heliothermal propulsion system and a flywheel orientation and stabilization system

Published: 18.05.2021

Authors: Zhumaev Z.S.

Published in issue: #5(113)/2021

DOI: 10.18698/2308-6033-2021-5-2078

Category: Aviation and Rocket-Space Engineering | Chapter: Design, construction and production of aircraft

    nanosatellite, CubeSat, propulsion, constellation of satellites, helioconcentrator, attitude determination and control system
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