NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Ejecta Generation and Redistribution on 433 Eros: Modeling Ejecta Launch ConditionsThe NEAR-Shoemaker mission to asteroid 433 Eros presents an unprecedented opportunity to gain fundamental new knowledge about the processes governing regolith formation and redistribution on small bodies. NEAR-Shoemaker’s high-resolution imaging of the surface of Eros makes the asteroid a valuable and heretofore unparalleled laboratory for the detailed study of impact ejecta reaccretion and regolith redistribution on low-gravity (of order 10-3 g) objects. Regolith is produced on asteroids by impact cratering, and the existence of regolith on the smallest solar system bodies supports the view that some of the ejecta from impact events on such objects may be retained. Impact craters and retained ejecta on low-gravity objects like Eros represent valuable natural laboratories for evaluating various models of impact cratering processes, since they may present crater structures or ejecta features that either do not form or are hidden on higher-gravity bodies like the Moon. Further, quantifying the extent to which impact processes generate and redistribute regoliths on small body surfaces (excavation depths, retained fraction, turnover timescales, etc.) is pivotal to the issue of how to relate meteoritical samples to their asteroidal parent bodies when surficial processes ( i.e., “space weathering”) may disguise or cover up underlying material and confound the ability of remote sensing techniques to provide reliable mineralogical assays of the parent objects. The rich variety of data on Eros’ regolith properties and distribution returned by NEAR-Shoemaker now require detailed analysis in order to take full advantage of the clues these observations offer for elucidating details of the impact cratering process on small bodies. Complicating simple interpretations of crater and ejecta morphology are dynamical effects on ejecta emplacement resulting from Eros’ irregular shape, rapid (5.27 hr) rotation, and low gravity. Figure 1 shows the very different ejecta deposit morphology that can result if the effects of rotation alone are neglected. Considering the additional complicating factors of Eros’ irregular shape and complex gravitational field, simple calculations of the extent and thickness of ejecta blankets and the spatial distribution of ejecta blocks from basic crater scaling laws or numerical hydrocodes alone do not suffice. In order to fully interpret the suite of NEAR-Shoemaker observations of regolith features across the surface of Eros and to evaluate various impact models for specific craters on the asteroid, detailed dynamical modeling of the deposition of crater ejecta from those craters is required. Here, I describe some modifications and improvements to the dynamical model being used for these studies.
Document ID
20040059601
Acquisition Source
Johnson Space Center
Document Type
Extended Abstract
Authors
D D Durda
(Southwest Research Institute San Antonio, United States)
Date Acquired
August 21, 2013
Publication Date
March 16, 2004
Publication Information
Publication: Lunar and Planetary Science XXXV: Asteroids, Meteors, and Comets
Publisher: Lunar and Planetary Institute
Subject Category
Lunar and Planetary Science and Exploration
Report/Patent Number
LPSC-2004-1096
LPI-Contrib-1197
Meeting Information
Meeting: 35th Lunar and Planetary Science Conference (LPSC)
Location: Houston, TX
Country: US
Start Date: March 15, 2004
End Date: March 19, 2004
Sponsors: Lunar and Planetary Institute, National Aeronautics and Space Administration
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available