NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Performance of an Annular Linear Induction Pump with Applications to Space Nuclear Power SystemsResults of performance testing of an annular linear induction pump are presented. The pump electromagnetically pumps liquid metal through a circuit specially designed to allow for quantification of the performance. Testing was conducted over a range of conditions, including frequencies of 33, 36, 39, and 60 Hz, liquid metal temperatures from 125 to 525 C, and input voltages from 5 to 120 V. Pump performance spanned a range of flow rates from roughly 0.16 to 5.7 L/s (2.5 to 90 gpm), and pressure head less than 1 to 90 kPa (less than 0.145 to 13 psi). The maximum efficiency measured during testing was slightly greater than 6%. The efficiency was fairly insensitive to input frequency from 33 to 39 Hz, and was markedly lower at 60 Hz. In addition, the efficiency decreased as the NaK temperature was raised. The performance of the pump operating on a variable frequency drive providing 60 Hz power compared favorably with the same pump operating on 60 Hz power drawn directly from the electrical grid.
Document ID
20100035100
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Polzin, Kurt A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Schoenfeld, Michael
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Pearson, J. Boise
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Webster, Kenneth
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Godfroy, Thomas
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Adkins, Harold E., Jr.
(Pacific Northwest National Lab. Richland, WA, United States)
Werner, James E.
(Idaho National Lab. Idaho Falls, ID, United States)
Date Acquired
August 25, 2013
Publication Date
July 25, 2010
Subject Category
Mechanical Engineering
Report/Patent Number
M10-0878
M10-0143
Meeting Information
Meeting: International Energy Conversion Engineering Conference
Location: Nashville, TN
Country: United States
Start Date: July 25, 2010
End Date: July 28, 2010
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available