Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
10694104 | Advances in Space Research | 2016 | 52 Pages |
Abstract
Laboratory simulations of landings with the test rig suggest that a large impact penetrometer under certain circumstances could absorb a significant amount of the elastic energy of the spacecraft possibly aiding landing. Alternatively a small impact penetrometer would allow the spacecraft to bounce freely off the surface to make a measurement at another location.
Related Topics
Physical Sciences and Engineering
Earth and Planetary Sciences
Space and Planetary Science
Authors
M.D. Paton, S.F. Green, A.J. Ball, J.C. Zarnecki, A. Hagermann,