• DocumentCode
    2544972
  • Title

    Launch packaging options for the PV power module cargo element

  • Author

    Hoberecht, Mark A. ; Vogt, Scott T.

  • Author_Institution
    NASA Lewis Res. Center, Cleveland, OH, USA
  • fYear
    1989
  • fDate
    6-11 Aug 1989
  • Firstpage
    295
  • Abstract
    The development of photovoltaic (PV) power module cargo element for the Space Station Freedom is discussed. The PV power module consists of several unique assemblies, each with its own function. These assemblies are combined in such a manner that functions are consolidated and packaging is efficient. Several packaging options for the PV power module cargo element are presented. These options are discussed in terms of their impact on the overall flight hardware manifest as determined by the various constraints. Space Station Freedom program considerations are also addressed
  • Keywords
    solar cell arrays; space vehicle power plants; PV power module; Space Station Freedom; assemblies; development; flight hardware manifest; packaging; solar cell arrays; space power; Assembly; Electronic packaging thermal management; Hardware; Multichip modules; NASA; Packaging machines; Space shuttles; Space stations; Thermal management of electronics; Transportation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Energy Conversion Engineering Conference, 1989. IECEC-89., Proceedings of the 24th Intersociety
  • Conference_Location
    Washington, DC
  • Type

    conf

  • DOI
    10.1109/IECEC.1989.74478
  • Filename
    74478