• DocumentCode
    1880146
  • Title

    A Gigawatt-level solar power satellite using Intensified Efficient Conversion Architecture

  • Author

    Komerath, Narayanan ; Dessanti, Brendan ; Shah, Shaan

  • Author_Institution
    Aerosp. Eng., Georgia Inst. of Technol., Atlanta, GA, USA
  • fYear
    2012
  • fDate
    3-10 March 2012
  • Firstpage
    1
  • Lastpage
    14
  • Abstract
    An Intensified Efficient Conversion Architecture (InCA) is proposed as a way of obtaining the high values of specific power needed to make Space Solar Power (SSP) viable. Unlike photovoltaic conversion, where converter mass scales linearly with power, gas turbine conversion offers strong advantages in specific power at the Gigawatt levels needed for SSP. Cycle efficiencies of 80 percent can be reached with intensifed sunlight, existing high-temperature materials and a helium gas cycle. By combining the passive radiator part of the thermal management system with the collector and antenna structures, specific power of 1.61 kWe/ kg is predicted for a converter satellite delivering 1 GWe of AC power at the ground. Prospects exist for up to 3.4 kWe/kg. This compares to the 0.15 kW/kg of the best present-day conceptions of photovoltaic power converters. This approach promises to make full-scale SSP economically viable much earlier than expected from prior work.
  • Keywords
    helium; photovoltaic power systems; power convertors; solar power satellites; space power generation; thermal management (packaging); AC power; He; antenna structures; collector structures; converter satellite; gas turbine conversion; intensified efficient conversion architecture; passive radiator; photovoltaic conversion; photovoltaic power converters; solar power satellite; space solar power; thermal management system; Computer architecture; Earth; Engines; Heating; Orbits; Satellites; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2012 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4577-0556-4
  • Type

    conf

  • DOI
    10.1109/AERO.2012.6187079
  • Filename
    6187079