• DocumentCode
    2981141
  • Title

    Lithium solid polymer batteries for aerospace

  • Author

    Teofilo, Vincent L. ; Nadell, Joel N.

  • Author_Institution
    Lockheed Martin Missiles & Space, Sunnyvale, CA, USA
  • Volume
    1
  • fYear
    1997
  • fDate
    27 Jul-1 Aug 1997
  • Firstpage
    1
  • Abstract
    Lockheed Martin Missiles and Space and Ultralife Batteries, Inc. are developing batteries for spacecraft and launchers based on Li-ion solid-polymer-electrolyte cell technology. These cells utilize a carbon anode, a manganese dioxide cathode and a solid polymer electrolyte. Electrode and electrolyte layers are thin and flexible. The electrode assembly is easily fabricated into thin, flat prismatic shapes using ordinary lamination techniques and is hermetically sealed in thin foil packaging. Cells ranging in capacity from 4 Ah to 50 Ah have been designed and are in development testing. The packaged cells have specific energies in excess of 100 Wh/kg. Prototype 30 volt batteries have also been designed and are being assembled and tested along with the critical battery cell charge management controllers needed to recharge all cells to full capacity while preventing overvoltage damage. The major results of this development effort are reviewed and the key issues for advancing this technology to flight qualification demonstrations are discussed
  • Keywords
    aerospace; anodes; cathodes; electrochemical electrodes; laminations; lithium; secondary cells; solid electrolytes; space vehicle power plants; 30 V; C anode; Li; Li-MnO2; Li-ion solid-polymer-electrolyte cell; Lockheed Martin Missiles and Space; MnO2 cathode; Ultralife Batteries; aerospace; battery cell charge management controllers; carbon anode; electrode assembly; flat prismatic shapes; flight qualification demonstrations; hermetically sealed; lamination techniques; launchers; lithium solid polymer batteries; manganese dioxide cathode; overvoltage damage prevention; spacecraft; thin foil packaging; Assembly; Batteries; Electrodes; Lithium; Missiles; Packaging; Polymers; Solids; Space technology; Testing;
  • 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.1997.659147
  • Filename
    659147