| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 8142695 | Planetary and Space Science | 2016 | 8 Pages |
Abstract
The simulation shows that the outbound velocity vector and the lander rotation were formed immediately at touch-down during the first 1.5Â s. The outbound velocity vector is found to be formed by the ground slope and the lander damping characteristic, especially the nearly horizontal flight out.
Keywords
Related Topics
Physical Sciences and Engineering
Earth and Planetary Sciences
Geophysics
Authors
Reinhard Roll, Lars Witte,