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AbstractAbstract
[en] Steady plane thermal detonations proceeding through coarse fuel-coolant mixtures have been predicted to exhibit pressures of /approximately equals/10/sup 4/ bar for UO/sub 2//Na and /approximately equals/10/sup 3/ bar for Sn/H/sub 2/O. This paper presents a few key results of some parametric calculations of steady plane thermal detonations, and in addition offer some broader comments. 33 refs
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Source
Anon; p. 1554-1567; 1979; p. 1554-1567; American Nuclear Society; LaGrange Park, IL; International meeting on fast reactor safety technology; Seattle, WA, USA; 19 - 23 Aug 1979
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Book
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Conference
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