Experimental ejection angles for oblique impacts: Implications for the subsurface flow-field
Citation
Anderson, J. L., Schultz, P. H., & Heineck, J. T. (2004). Experimental ejection angles for oblique impacts: Implications for the subsurface flow‐field. Meteoritics & Planetary Science, 39(2), 303-320.Publisher
The Meteoritical SocietyJournal
Meteoritics & Planetary ScienceDescription
From the proceedings of the Workshop on Impact Cratering: Bridging the Gap between Modeling and Observations held in February 2003 at the Lunar and Planetary Institute in Houston, Texas.Additional Links
https://meteoritical.org/Abstract
A simple analytical solution for subsurface particle motions during impact cratering is useful for tracking the evolution of the transient crater shape at late times. A specific example of such an analytical solution is Maxwells Z-Model, which is based on a point-source assumption. Here, the parameters for this model are constrained using measured ejection angles from both vertical and oblique experimental impacts at the NASA Ames Vertical Gun Range. Data from experiments reveal that impacts at angles as high as 45 degrees to the targets surface generate subsurface flow-fields that are significantly different from those created by vertical impacts. The initial momentum of the projectile induces a subsurface momentum-driven flow-field that evolves in three dimensions of space and in time to an excavation flow-field during both vertical and oblique impacts. A single, stationary pointsource model (specifically Maxwells Z-Model), however, is found inadequate to explain this detailed evolution of the subsurface flow-field during oblique impacts. Because 45 degrees is the most likely impact angle on planetary surfaces, a new analytical model based on a migrating point-source could prove quite useful. Such a model must address the effects of the subsurface flow-field evolution on crater excavation, ejecta deposition, and transient crater morphometry.Type
Proceedingstext
Language
enISSN
1945-5100ae974a485f413a2113503eed53cd6c53
10.1111/j.1945-5100.2004.tb00342.x