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Primary zinc-air batteries for space powerPrismatic HR and LC cells and batteries were built and tested, and they performed well with respect to the program goals of high capacity and high rate capability at specific energies. The HR batteries suffered reduced utilizations owing to dryout at the 2 and 3 A rates for the 50 C tests owing to the requirement for forced convection. The LC batteries suffered reduced utilizations under all conditions owing to the chimney effect at 1 G, although this effect would not occur at 0 G. An empirical model was developed which accurately predicted utilizations and average voltages for single cells, although thermal effects encountered during battery testing caused significant deviations, both positive and negative, from the model. Based on the encouraging results of the test program, we believe that the zinc-air primary battery of a flat, stackable configuration can serve as a high performance and safe power source for a range of space applications.
Document ID
19920013505
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bragg, Bobby J.
(Metal Air Technology Systems International, Inc., Atlanta GA., United States)
Bourland, Deborah S.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Merry, Glenn
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Putt, Ron
(Metal Air Technology Systems International, Inc., Atlanta GA., United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1992
Publication Information
Publication: NASA. Marshall Space Flight Center, The 1991 NASA Aerospace Battery Workshop
Subject Category
Energy Production And Conversion
Accession Number
92N22748
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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