Design of lunar gravity assist for the BepiColombo mission to mercury

被引：0

作者：

Campagnola, S ^{[1
]}

Jehn, R ^{[1
]}

Van Damme, CC ^{[1
]}

机构：

[1] European Space Agcy, European Space Operat Ctr, Miss Anal Off, D-64293 Darmstadt, Germany

来源：

Spaceflight Mechanics 2004, Vol 119, Pt 1-3 | 2005年 / 119卷

关键词：

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

The BepiColombo mission to Mercury makes use of a lunar gravity-assist to increase the payload mass into the final orbit. The swing-by of the Moon is designed such that the highest velocity in the suitable direction is obtained. Furthermore a phasing loop strategy is investigated, which opens a 5-month launch window. Taking into account the luni-solar perturbations, the launch window has to be closed frequently, but launch opportunities remain from May to September 2012.

引用

页码：427 / 441

页数：15

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