• DocumentCode
    1707113
  • Title

    Improved sodium sulfur LEO performance

  • Author

    De Gruson, J.A. ; Silvey, R.L.

  • Author_Institution
    Eagle-Picher Ind. Inc., Joplin, MO, USA
  • fYear
    1992
  • Firstpage
    399
  • Lastpage
    402
  • Abstract
    Improved sodium sulfur technology has been developed for low Earth orbit (LEO) space applications. In addition to a high charge/discharge rate capability, improvements have been made relative to sodium availability, cathode corrosion resistance, cell resistance, and electrolyte performance. Cell sizes ranging from 10-Ah capacity to 55-Ah have been built and tested with the 55-Ah cell being utilized as a standard. A long cycle life of 10000 cycles without capacity loss has been demonstrated. The design is such that 60% and 80% depth of discharge are attainable at LEO rates and a specific energy of 186 Wh/kghas been demonstrated. A limited number of safety tests have been conducted on the final designed cells. These test have been successful in that no catastrophic failures have occurred
  • Keywords
    cathodes; electrochemical electrodes; life testing; secondary cells; sodium; space vehicle power plants; sulphur; LEO performance; Na-S; cathode corrosion resistance; cell resistance; depth of discharge; electrolyte performance; high charge/discharge rate capability; long cycle life; low Earth orbit; safety tests; sodium availability; space applications; Aerospace industry; Availability; Cathodes; Contracts; Corrosion; Electric resistance; Low earth orbit satellites; Power supplies; Space technology; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Power Sources Symposium, 1992., IEEE 35th International
  • Conference_Location
    Cherry Hill, NJ
  • Print_ISBN
    0-7803-0552-3
  • Type

    conf

  • DOI
    10.1109/IPSS.1992.281972
  • Filename
    281972