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Technology Projections for Solar Dynamic PowerSolar Dynamic power systems can offer many potential benefits to Earth orbiting satellites including high solar-to-electric efficiency, long life without performance degradation, and high power capability. A recent integrated system test of a 2 kilowatt SD power system in a simulated space environment has successfully demonstrated technology readiness for space flight. Conceptual design studies of SD power systems have addressed several potential mission applications: a 10 kilowatt LEO satellite, a low power Space Based Radar, and a 30 kilowatt GEO communications satellite. The studies show that with moderate component development, SD systems can exhibit excellent mass and deployed area characteristics. Using the conceptual design studies as a basis, a SD technology roadmap was generated which identifies the component advances necessary to assure SD systems a competitive advantage for future NASA, DOD, and commercial missions.
Document ID
19990018826
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mason, Lee S.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1999
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA/TM-1999-208851
E-11473
NAS 1.15:208851
Report Number: NASA/TM-1999-208851
Report Number: E-11473
Report Number: NAS 1.15:208851
Meeting Information
Meeting: Space Technology and Applications
Location: Albuquerque, NM
Country: United States
Start Date: January 31, 1999
End Date: February 4, 1999
Sponsors: NASA Headquarters, Lockheed Martin Corp., Department of the Air Force, Boeing Co., Department of Energy
Funding Number(s)
PROJECT: RTOP 632-1A-1D
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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