| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 8055650 | Acta Astronautica | 2018 | 9 Pages |
Abstract
The purpose of the present study is to find optimized safe separation conditions to limit the in-orbit collision risk following the injection of many objects on very close orbits in a short-delay mission.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
D.-DA.-A. Handschuh, E. Bourgeois,