| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1717062 | Acta Astronautica | 2007 | 6 Pages |
Abstract
A correlation between planning for CEV and surface system requirements demands an integrated approach. Launch and orbital transfer means must be analyzed in parallel with comprehensive payload needs and element design options. Accordingly, studies should address a variety of option drivers and alternatives, including:
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Larry Bell,