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Solar power satellite rectenna design study: Directional receiving elements and parallel-series combining analysisRectenna conversion efficiencies (RF to dc) approximating 85 percent were demonstrated on a small scale, clearly indicating the feasibility and potential of efficiency of microwave power to dc. The overall cost estimates of the solar power satellite indicate that the baseline rectenna subsystem will be between 25 to 40 percent of the system cost. The directional receiving elements and element extensions were studied, along with power combining evaluation and evaluation extensions.
Document ID
19790007868
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gutmann, R. J.
(Rensselaer Polytechnic Inst. Troy, NY, United States)
Borrego, J. M.
(Rensselaer Polytechnic Inst. Troy, NY, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1978
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-CR-151866
Report Number: NASA-CR-151866
Accession Number
79N16039
Funding Number(s)
CONTRACT_GRANT: NAS9-15453
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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