Article ID Journal Published Year Pages File Type
10694104 Advances in Space Research 2016 52 Pages PDF
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
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