DocumentCode :
2427292
Title :
Lunar Prospector 5 Ah Super NiCd battery performance characteristics
Author :
Mason, Gary E. ; Daman, Marsha E. ; Waller, James S. ; Hayden, Jeffrey W.
Author_Institution :
Lockheed Martin Missiles & Space, Sunnyvale, CA, USA
fYear :
1998
fDate :
13-16 Jan 1998
Firstpage :
103
Lastpage :
106
Abstract :
Lunar Prospector uses a 5 Ah Super NiCd twenty-two cell battery in a battery dominated satellite bus architecture. The battery is tasked heavily in a “LEO”-type cycle regime. The lunar orbit is 118 minutes, with an eclipse of 47 minutes maximum. The battery will experience approximately 3500 cycles between 50 and 60 percent DOD (depth of discharge). The Super NiCd battery type was selected because of its robust cycle life performance. The charge control used for this mission is a charge to a temperature compensated constant voltage method. Substantial characterization testing was performed to verify battery performance in this rigorous regime. Lunar Prospector is one of the Discovery series of NASA missions which is accomplished at minimal cost
Keywords :
cadmium; nickel; secondary cells; space vehicle power plants; LEO-type cycle regime; Lunar Prospector; NASA mission; Ni-Cd; Super NiCd battery; characterization testing; charge control; depth of discharge; performance characteristics; robust cycle life performance; satellite bus architecture; temperature compensated constant voltage method; Batteries; Moon; NASA; Performance evaluation; Robustness; Satellites; Temperature control; Testing; US Department of Defense; Voltage control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Battery Conference on Applications and Advances, 1998., The Thirteenth Annual
Conference_Location :
Long Beach, CA
ISSN :
1089-8182
Print_ISBN :
0-7803-4098-1
Type :
conf
DOI :
10.1109/BCAA.1998.653849
Filename :
653849
Link To Document :
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