| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1717307 | Acta Astronautica | 2006 | 8 Pages |
Abstract
This particular mission is going very far from the Sun imposing hard and specific constraints such as very low mass allocation, limited volume and limited power allocations. Taking into account these constraints, specific developments have been made, based principally on “off-the-shelf” component procurement, the use of past experience and also the use of highly integrated electronic components, available only in commercial version.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Andre Debus, Denis Moura,