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Lightweight, direct-radiating nickel hydrogen batteriesTwo battery module configurations were developed which, in addition to integrating cylindrical nickel hydrogen (NiH2) cells into batteries, provide advances in the means of mounting, monitoring and thermal control of these cells. The main difference between the two modules is the physical arrangement of the cells: vertical versus horizontal. Direct thermal radiation to deep space is accomplished by substituting the battery structure for an exterior spacecraft panel. Unlike most conventional nickel-cadmium (NiCd) and NiH2 batteries, the cells are not tightly packed together; therefore ancillary heat conducting media to outside radiating areas, and spacecraft deck reinforcements for high mass concentration are not necessary. Testing included electrical characterization and a comprehensive regime of environmental exposures. The designs are flexible with respect to quantity and type of cells, orbit altitude and period, power demand profile, and the extent of cell parameter monitoring. This paper compares the characteristics of the two battery modules and summarizes their performance.
Document ID
19870001663
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Metcalfe, J. R.
(Canadian Astronautics Ltd. Ottawa Ontario, Canada)
Date Acquired
August 13, 2013
Publication Date
September 1, 1986
Publication Information
Publication: NASA. Goddard Space Flight Center The 1985 Goddard Space Flight Center Battery Workshop (date)
Subject Category
Electronics And Electrical Engineering
Accession Number
87N11096
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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