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
Engineering
Aerospace Engineering
Authors
B.G. Marchand, S.K. Scarritt, T.A. Pavlak, K.C. Howell,