NASA/TM-2007-214851, Polzin, K.A., Liquid-Metal Pump Technologies for Nuclear Surface Power, George C. Marshall Space Flight Center, Marshall Space Flight Center, AL 35812, National Aeronautics and Space Administration, Washington, DC 20546–0001, March 2007, pp. 36, Format(s): PDF 676k |
Multiple 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.
| Keywords: | liquid-metal pumps, electromagnetic pumps, magnetohydrodynamics, nonnuclear testing. |
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| Subjects: | Astronautics: Spacecraft Propulsion And Power |
| ID Code: | 745 |
| Deposited On: | 24 May 2007 |