Article ID Journal Published Year Pages File Type
8057077 Acta Astronautica 2013 14 Pages PDF
Abstract
► The dynamical aspects of precision entry in the three-body problem are considered. ► Interaction between the entry dispersion manifolds and the Hill sphere studied. ► An example involving the Orion trans-Earth injection sequence is presented. ► Third body effects harnessed to reduce the overall cost of global precision entry.
Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
Authors
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