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
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