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The solar power satellite concepts: The past decade and the next decadeResults of studies on the solar power satellite concept are summarized. The basic advantages are near continuous access to sunlight and freedom from atmospheric effects and cloud cover. The systems definition studies consider photovoltaic and thermal energy conversion systems and find both to be technically feasible, with the photovoltaic approach preferred. A microwave test program is under way which will provide quantitative data on critical parameters, including beam forming and steering accuracy. Ballistic and winged launch vehicles are defined for the transportation of construction materials, with the shuttle expected to provide low cost transportation to and from space. A reference system is outlined for evaluating the concept in terms of environmental and other considerations. Preliminary estimates of natural resource requirements and energy payback intervals are encouraging.
Document ID
19800016865
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kraft, C. C., Jr.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1979
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-TM-81000
JSC-14898
Meeting Information
Meeting: AIAA Ann. Meeting and Tech. Display
Location: Washington, DC
Country: United States
Start Date: February 6, 1979
End Date: February 8, 1979
Accession Number
80N25360
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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