Article ID Journal Published Year Pages File Type
10680853 Acta Astronautica 2014 15 Pages PDF
Abstract
► An end-to-end pole-sitter mission is presented for continuous Earth polar observation. ► A near-term, SEP and a far-term, hybrid solar sail/SEP mission are considered. ► Optimal pole-sitter orbits and transfers from LEO are designed for a Soyuz/Ariane launch. ► A mass budget analysis trades off mission lifetime and payload mass. ► Transfers between north and south pole-sitters are designed to overcome polar winters.
Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
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