| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 785508 | International Journal of Non-Linear Mechanics | 2016 | 14 Pages |
Abstract
Our simulations aim to identify regions where the debris can temporarily orbit around the asteroid or rather escape from it or fall back on the surface. These results give an important information on where a spacecraft could be safely stay after the end of the process which has produced the debris.
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Physical Sciences and Engineering
Engineering
Mechanical Engineering
Authors
Massimo Vetrisano, Alessandra Celletti, Giuseppe Pucacco,