| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 8057077 | Acta Astronautica | 2013 | 14 Pages |
Abstract
⺠The dynamical aspects of precision entry in the three-body problem are considered. ⺠Interaction between the entry dispersion manifolds and the Hill sphere studied. ⺠An example involving the Orion trans-Earth injection sequence is presented. ⺠Third body effects harnessed to reduce the overall cost of global precision entry.
Related Topics
Physical Sciences and Engineering
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Aerospace Engineering
Authors
B.G. Marchand, S.K. Scarritt, T.A. Pavlak, K.C. Howell,