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Emergency cooling analysis for the loss of coolant malfunctionThis report examines the dynamic response of a conceptual space power fast-spectrum lithium cooled reactor to the loss of coolant malfunction and several emergency cooling concepts. The results show that, following the loss of primary coolant, the peak temperatures of the center most 73 fuel elements can range from 2556 K to the region of the fuel melting point of 3122 K within 3600 seconds after the start of the accident. Two types of emergency aftercooling concepts were examined: (1) full core open loop cooling and (2) partial core closed loop cooling. The full core open loop concept is a one pass method of supplying lithium to the 247 fuel pins. This method can maintain fuel temperature below the 1611 K transient damage limit but requires a sizable 22,680-kilogram auxiliary lithium supply. The second concept utilizes a redundant internal closed loop to supply lithium to only the central area of each hexagonal fuel array. By using this method and supplying lithium to only the triflute region, fuel temperatures can be held well below the transient damage limit.
Document ID
19720007954
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Peoples, J. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Nuclear Engineering
Report/Patent Number
NASA-TM-X-2464
E-6520
Report Number: NASA-TM-X-2464
Report Number: E-6520
Accession Number
72N15604
Funding Number(s)
PROJECT: RTOP 112-27
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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