• DocumentCode
    1148372
  • Title

    Leasecraft Power System Leasecraft Power System

  • Author

    Chetty, P.R.K.

  • Author_Institution
    Fairchild Space Company
  • Issue
    3
  • fYear
    1985
  • fDate
    5/1/1985 12:00:00 AM
  • Firstpage
    420
  • Lastpage
    426
  • Abstract
    Various building blocks of the Fairchild Leasecraft Power System are described in detail after a brief description of the evolution of the Leasecraft spacecraft. The principle of maximum power transfer from a solar cell array has been employed in the power system advantageously. Results of detailed tradeoff studies are presented which led to the selection of the decentralized regulation concept utilizing a nondissipative unregulated main (power) bus approach. Finally the main features of the Leasecraft Power System, i.e., flexibility, reliability, input and output electrical characteristics, etc. are presented.
  • Keywords
    Aircraft manufacture; Industrial power systems; NASA; Photovoltaic cells; Power system interconnection; Power system reliability; Power systems; Space shuttles; Space vehicles; Testing;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1985.310573
  • Filename
    4104072