Abstract
Space debris is increasingly concerned by aerospace engineers and scientists. The evolution of an orbital debris cloud, the collision probability between of debris and a spacecraft, and the damage evaluation of spacecraft when impacted by space debris are studied in this work. A hypervelocity impact model for honeycomb panel is proposed. Under considering secondary debris, the survivability of spacecraft impacted by space debris is finally investigated.
| Original language | English |
|---|---|
| Pages (from-to) | 282-285 |
| Number of pages | 4 |
| Journal | Nuclear Physics B - Proceedings Supplements |
| Volume | 166 |
| DOIs | |
| State | Published - Apr 2007 |
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