DocumentCode
321493
Title
Ultra low temperature batteries for Martian applications
Author
Deligiannis, F. ; Frank, H. ; Davies, E. ; Russell, P.G. ; Reddy, T.B.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume
1
fYear
1997
fDate
27 Jul-1 Aug 1997
Firstpage
72
Abstract
The Mars Microprobes are a secondary payload on the 1998 Mars Surveyor Lander Mission. The power source for the Microprobes will be two lithium primary batteries. The batteries will provide power for all the Microprobe instruments and data relays during all phases of the mission. The batteries will be designed to survive the peak landing shock that may reach 80,000 g and to withstand the stringent Martian surface temperatures (-80°C). Primary lithium batteries were selected for the Microprobes based on the high specific energy and the promising low temperature performance. Modifications to existing lithium primary cells were made to develop a battery that met all requirements. This paper describes the cell/battery design and provides test results obtained during the various phases of development
Keywords
Mars; aerospace testing; electrochemistry; lithium; primary cells; space vehicle power plants; -80 C; Li; Li primary batteries; Mars Microprobes; Martian applications; Martian surface temperatures; battery design; low temperature performance; peak landing shock; performance testing; space power; specific energy; ultra-low temperature batteries; Batteries; Instruments; Laboratories; Lithium; Mars; Payloads; Probes; Propulsion; Soil; Temperature;
fLanguage
English
Publisher
ieee
Conference_Titel
Energy Conversion Engineering Conference, 1997. IECEC-97., Proceedings of the 32nd Intersociety
Conference_Location
Honolulu, HI
Print_ISBN
0-7803-4515-0
Type
conf
DOI
10.1109/IECEC.1997.659162
Filename
659162
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