• 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