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| Research Progress in Shape Effect of Space Debris under Hypervelocity Impact |
| Received:July 23, 2019 Revised:September 23, 2019 |
| View Full Text View/Add Comment Download reader |
| DOI：10.7643/issn.1672-9242.2020.03.008 |
| KeyWord:hypervelocity impact non-spherical shape effect ballistic limit |
| Author | Institution |
| SONG Guang-ming |
Beijing Institute of Spacecraft Environment Engineering, Beijing , China |
| WU Qiang |
Beijing Institute of Spacecraft Environment Engineering, Beijing , China |
| LI Ming |
China Academy of Space Technology, Beijing , China |
| GONG Zi-zheng |
Beijing Institute of Spacecraft Environment Engineering, Beijing , China |
| XIANG Shu-hong |
Beijing Institute of Spacecraft Environment Engineering, Beijing , China |
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| Abstract: |
| The research status and latest progress in the field of shape effect under hypervelocity impact conditions by researchers at home and abroad in recent years were introduced, on the basis of analyzing the technical routes for studying the shape effect of space debris under hypervelocity impact conditions at home and abroad. Based on the current situation of space debris protection engineering requirements of domestic spacecraft, the development direction of the shape effect research of space debris under hypervelocity impact conditions in China was discussed in combination with the research status and the latest progress. |
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