NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Liquid-Metal Pump Technologies for Nuclear Surface PowerMultiple liquid-metal pump options are reviewed for the purpose of determining the technologies that are best suited for inclusion in a nuclear reactor thermal simulator intended to test prototypical space nuclear system components. Conduction, induction, and thermoelectric electromagnetic pumps are evaluated based on their performance characteristics and the technical issues associated with incorporation into a reactor system. The thermoelectric pump is recommended for inclusion in the planned system at NASA MSFC based on its relative simplicity, low power supply mass penalty, flight heritage, and the promise of increased pump efficiency over earlier flight pump designs through the use of skutterudite thermoelectric elements.
Document ID
20070022272
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Polzin, K. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 23, 2013
Publication Date
March 1, 2007
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA/TM-2007-214851
M-1182
Report Number: NASA/TM-2007-214851
Report Number: M-1182
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available