DocumentCode :
3201270
Title :
Lithium ion batteries for Mars exploration missions
Author :
Ratnakumar, B.V. ; Smart, M.C. ; Byers, J. ; Ewell, R. ; Surampudi, S.
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear :
1999
fDate :
1999
Firstpage :
51
Lastpage :
54
Abstract :
The upcoming NASA missions aimed at exploring our Planetary system require batteries that can operate at extreme operating temperatures, with high specific energy and energy densities. Conventional aerospace rechargeable battery systems are inadequate to meet the demands. Lithium ion rechargeable batteries are thus being chosen for these missions. The Mars 2001 (Mars Surveyor Program MSP 01) Lander and the 2003 Mars Sample Return/Athena Rover are among the first of NASA´s missions to utilize the lithium ion technology. One common feature of these two missions is the need for the battery to operate well at sub-zero temperatures (down to -30°C), at moderate rates of charge and discharge. Elsewhere are therefore focussing on improving the low temperature performance of Li ion cells. Preliminary evaluations of the prototype cells reveal the adequacy of their performance to the needs of these missions
Keywords :
Mars; electrochemistry; lithium; secondary cells; space vehicle power plants; Li-ion secondary batteries; Mars exploration missions; NASA missions; aerospace rechargeable battery systems; charge rates; discharge rates; energy density; extreme operating temperature; space power; specific energy; sub-zero temperatures; Batteries; Electric shock; Laboratories; Lithium; Mars; Nickel; Probes; Propulsion; Space technology; Temperature;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Battery Conference on Applications and Advances, 1999. The Fourteenth Annual
Conference_Location :
Long Beach, CA
ISSN :
1089-8182
Print_ISBN :
0-7803-4967-9
Type :
conf
DOI :
10.1109/BCAA.1999.795965
Filename :
795965
Link To Document :
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