Article ID Journal Published Year Pages File Type
8057003 Acta Astronautica 2014 9 Pages PDF
Abstract
The methodology has then been applied to select design strategies (additional local shielding, relocation of components) to improve S/C protection with respect to MMOD. The results of the analyses conducted on the improved design show a reduction of the vulnerability index of about 18%.
Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
Authors
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