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Design of a Mechanical NaK Pump for Fission Space PowerAlkali liquid metal cooled fission reactor concepts are under development for spaceflight power requirements. One such concept utilizes a sodium-potassium eutectic (NaK) as the primary loop working fluid, which has specific pumping requirements. Traditionally, electromagnetic linear induction pumps have been used to provide the required flow and pressure head conditions for NaK systems but they can be limited in performance, efficiency, and number of available vendors. The objective of the project was to develop a mechanical NaK centrifugal pump that takes advantages of technology advances not available in previous liquid metal mechanical pump designs. This paper details the design, build, and performance test of a mechanical NaK pump developed at NASA Marshall Space Flight Center. The pump was designed to meet reactor cooling requirements using commercially available components modified for high temperature NaK service.
Document ID
20110015702
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Mireles, Omar R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Bradley, David E.
(Yetispace, Inc. Huntsville, AL, United States)
Godfroy, Thomas
(MTC Technologies Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
August 1, 2011
Subject Category
Nuclear Physics
Report/Patent Number
M11-0550
Report Number: M11-0550
Meeting Information
Meeting: A1AA IECEC Conference
Location: San Diego, CA
Country: United States
Start Date: August 1, 2011
End Date: August 4, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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