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Hypervelocity Impact Energy Loss and Track Shape in Aerogels: Theory and ExperimentWe have developed and tested a theoretical model of impact cratering in aerogels that derives the impact crater dimensions directly from the energy and momentum deposition of the projectile. In this paper, our work is outlined.
Document ID
20040065857
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Dominguez, G. (California Univ. Berkeley, CA, United States)
Westphal, A. J. (California Univ. Berkeley, CA, United States)
Jones, S. M. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Phillips, M. L. F. (Pleasanton Ridge Research Corp. Hayward, CA, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2004
Publication Information
Publication: Lunar and Planetary Science XXXV: Big Dust, Little Dust, and Aerogel
Subject Category
Lunar And Planetary Science And Exploration
Distribution Limits
Public
Copyright
Public Use Permitted.
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IDRelationTitle20040065855Collected WorksLunar and Planetary Science XXXV: Big Dust, Little Dust, and Aerogel
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