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The effect of impact angle on craters formed by hypervelocity particlesThe Space Power Institute (SPI) at Auburn University has conducted experiments on the effects of impact angle on crater morphology and impactor residue retention for hypervelocity impacts. Copper target plates were set at angles of 30 deg, 45 deg, 60 deg, and 75 deg from the particle flight path. For the 30 deg and 45 deg impacts, in the velocity regime greater than 8 km s(exp -1) the resultant craters are almost identical to normal incidence impacts. The only difference found was in the apparent distribution of particle residue within the crater, and further research is needed to verify this. The 60 deg and 75 deg impacts showed marked differences in crater symmetry, crater lip shape, and particle residue distribution in the same velocity regime. Impactor residue shock fractionation effects have been quantified in first-order. It is concluded that a combination of analysis techniques can yield further information on impact velocity, direction, and angle of incidence.
Document ID
19950017419
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hill, David C.
(Auburn Univ. AL, United States)
Rose, M. Frank
(Auburn Univ. AL, United States)
Best, Steve R.
(Auburn Univ. AL, United States)
Crumpler, Michael S.
(Auburn Univ. AL, United States)
Crawford, Gary D.
(Auburn Univ. AL, United States)
Zee, Ralph H.-C.
(Auburn Univ. AL, United States)
Bozack, Michael J.
(Auburn Univ. AL, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1995
Publication Information
Publication: NASA. Langley Research Center, LDEF: 69 Months in Space. Third Post-Retrieval Symposium, Part 1
Subject Category
Structural Mechanics
Accession Number
95N23839
Funding Number(s)
CONTRACT_GRANT: NAG1-1329
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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