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Online Oxide Contamination Measurement and Purification DemonstrationLiquid metal sodium-potassium (NaK) has advantageous thermodynamic properties indicating its use as a fission reactor coolant for a surface (lunar, martian) power system. A major area of concern for fission reactor cooling systems is system corrosion due to oxygen contaminants at the high operating temperatures experienced. A small-scale, approximately 4-L capacity, simulated fission reactor cooling system employing NaK as a coolant was fabricated and tested with the goal of demonstrating a noninvasive oxygen detection and purification system. In order to generate prototypical conditions in the simulated cooling system, several system components were designed, fabricated, and tested. These major components were a fully-sealed, magnetically-coupled mechanical NaK pump, a graphite element heated reservoir, a plugging indicator system, and a cold trap. All system components were successfully demonstrated at a maximum system flow rate of approximately 150 cc/s at temperatures up to 550 C. Coolant purification was accomplished using a cold trap before and after plugging operations which showed a relative reduction in oxygen content.
Document ID
20110022666
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Publication (TP)
Authors
Bradley, D. E.
(Yetispace, Inc. Huntsville, AL, United States)
Godfroy, T. J.
(Maximum Technology Corp. Huntsville, AL, United States)
Webster, K. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Garber, A. E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Polzin, K. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Childers, D. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
October 1, 2011
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA/TP-2011-216473
M-1322
Distribution Limits
Public
Copyright
Public Use Permitted.
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