• DocumentCode
    304167
  • Title

    The Bruno B. Rossi X-ray Timing Explorer (RXTE) battery design and performance

  • Author

    Jallice, Doris E. ; Ahmad, Anisa J. ; Rao, Gopalakrishna M.

  • Author_Institution
    NASA Goddard Space Flight Center, Greenbelt, MD, USA
  • Volume
    1
  • fYear
    1996
  • fDate
    11-16 Aug 1996
  • Firstpage
    421
  • Abstract
    The Bruno B. Rossi X-ray Timing Explorer (RXTE), a NASA astronomy satellite, was launched on December 30, 1995. The RXTE power system is a direct energy transfer system with two super nickel cadmium batteries and an eight segment silicon solar array connected directly to the main bus. The RXTE power system can provide up to 800 watts of load power. Provisions are incorporated into the power system electronics design for partially isolating any one battery in flight for individual battery charging or for fully isolating any one battery in flight for battery reconditioning. This paper describes the RXTE cell and battery ground test performance, and in-orbit battery operations and performance
  • Keywords
    aerospace testing; cadmium; nickel; photovoltaic power systems; secondary cells; solar cell arrays; solar cells; space vehicle power plants; Bruno B. Rossi X-ray Timing Explorer; NASA astronomy satellite; Ni-Cd; RXTE satellite power system; Si; battery charging; battery design; battery performance; battery reconditioning; direct energy transfer system; ground test performance; in-orbit battery operations; in-orbit performance; main bus; secondary batteries; solar array; space power; Astronomy; Batteries; Cadmium; Energy exchange; NASA; Nickel; Power systems; Satellites; Silicon; Timing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Energy Conversion Engineering Conference, 1996. IECEC 96., Proceedings of the 31st Intersociety
  • Conference_Location
    Washington, DC
  • ISSN
    1089-3547
  • Print_ISBN
    0-7803-3547-3
  • Type

    conf

  • DOI
    10.1109/IECEC.1996.552919
  • Filename
    552919