Abstract
Plenty of space debris are produced by human in space. They are a threat to the normal operation of in-orbit spacecrafts. So, it is necessary to develop a new material shielding structure with a good protection performance. Here, the impact properties of a cenosphere/aluminum matrix composite stuffed shield were investigated. Then, some data related to impact damage were obtained, and they were compared with those of a whipple protection structure using solid aluminum stuffed shield. On this basis, the feasibility of cenosphere/aluminum matrix composite material as a protection material for spacecraft was evaluated.
| Original language | English |
|---|---|
| Pages (from-to) | 141-145 |
| Number of pages | 5 |
| Journal | Zhendong yu Chongji/Journal of Vibration and Shock |
| Volume | 32 |
| Issue number | 18 |
| State | Published - 28 Sep 2013 |
| Externally published | Yes |
Keywords
- Cenosphere/aluminum matrix composite
- Hypervelocity impact
- Protection performance
- Space debris
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