• DocumentCode
    2784519
  • Title

    The Solar Probe Plus solar array development and design

  • Author

    Gaddy, Edward ; Decker, Rob ; Lockwood, Mary Kae ; Roufberg, Lew ; Knutzen, Gayle ; Marsh, Danielle

  • Author_Institution
    Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD, USA
  • fYear
    2010
  • fDate
    20-25 June 2010
  • Abstract
    The Solar Probe Plus (SPP) spacecraft will orbit as closely as 9.5 solar radii from the sun; so close that its thermal protection shield (TPS) will reach a peak temperature of 1,400C. To work in this environment, the solar array will use pressurized water cooling and operate in the penumbra formed by the TPS at a 68° angle of incidence. Even with these mitigations, the array will be subject to extremely high intensity and temperature. This paper will summarize the array´s environment, present a preliminary design, outline development plans and describe phase A test plans. This paper will summarize the array´s environment, present a preliminary design, outline development plans and describe phase A test plans.
  • Keywords
    solar cell arrays; solar heating; space vehicles; thermal resistance; pressurized water cooling; solar array; solar probe plus spacecraft; temperature 1400 C; thermal protection shield; Arrays; Electrostatics; Insulators; Materials; Resistance; Sun; Trajectory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Photovoltaic Specialists Conference (PVSC), 2010 35th IEEE
  • Conference_Location
    Honolulu, HI
  • ISSN
    0160-8371
  • Print_ISBN
    978-1-4244-5890-5
  • Type

    conf

  • DOI
    10.1109/PVSC.2010.5617077
  • Filename
    5617077