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Technology for satellite power conversionComponents were examined that will be needed for high frequency rectenna devices. The majority of the effort was spent on measuring the directivity and efficiency of the half-wave dipole antenna. It is felt that the antenna and diode should be roughly optimized before they are combined into a rectenna structure. An integrated low pass filter had to be added to the antenna structure in order to facilitate the field pattern measurements. A calculation was also made of the power density of the Earth's radiant energy as seen by satellites in Earth orbit. Finally, the feasibility of using a Metal-Oxide-Metal (MOM) diode for rectification of the received power was assessed.
Document ID
19870015987
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gouker, M. A.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Campbell, D. P.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Gallagher, J. J.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Date Acquired
September 5, 2013
Publication Date
June 30, 1987
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
A-3244
NASA-CR-181057
NAS 1.26:181057
Report Number: A-3244
Report Number: NASA-CR-181057
Report Number: NAS 1.26:181057
Accession Number
87N25420
Funding Number(s)
CONTRACT_GRANT: NAG3-282
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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