| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1716039 | Acta Astronautica | 2009 | 8 Pages |
Abstract
The aim of this work is to develop simplified model of space debris particle collision on solid structures, which would provide closed form solution formulas for determining crater depth, radius and ejected mass being functions of impactor mass, speed and material of both impactor and target. The model will be verified with results of experiments.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
N.N. Smirnov, K.A. Kondratyev,