1996
DOI: 10.2172/273765
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General-Purpose Heat Source: Research and development program: Cold-Process Verification Test Series

Abstract: Los Alamos National Laboratory is operated by the University ofCal@mia fur the United States Department of Energy under contract W-7405-ENG36.

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Cited by 5 publications
(5 citation statements)
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“…The typical number of cracks range from 0 to 3 at this impact velocity. (26) The deformation of the clad is comparable to that observed in previous simulant-fueled, bare-clad impact tests. The maximum percent strain varies between 12 to 16 axially, and diametrically 6 to 18 in the vent cup, 6 to 18 in the girth weld area, and 5 to 9 in the shield cup.…”
Section: Sc0144 Impact Responsesupporting
confidence: 81%
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“…The typical number of cracks range from 0 to 3 at this impact velocity. (26) The deformation of the clad is comparable to that observed in previous simulant-fueled, bare-clad impact tests. The maximum percent strain varies between 12 to 16 axially, and diametrically 6 to 18 in the vent cup, 6 to 18 in the girth weld area, and 5 to 9 in the shield cup.…”
Section: Sc0144 Impact Responsesupporting
confidence: 81%
“…This has not been observed in other urania-fueled, bareclad impact tests. (26) The total number of observed cracks is also atypical. The typical number of cracks range from 0 to 3 at this impact velocity.…”
Section: Sc0144 Impact Responsementioning
confidence: 99%
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“…However, the magnitude of these weight fractions are very small in comparison to the weight fractions measured in the CPV tests (two to 9.2 times smaller). 15 2, and the other clads recovered from RTG-1 and RTG-2. The fraction of urania recovered from SC0107 in the +5600 mm range is almost twice that recovered from SC0076, SC0092, and SC0096.…”
Section: B Pellet Fragmentationmentioning
confidence: 97%