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Construction and testing of a space ready rectennaIn Feb. 1993, the Solar Power Satellite (SPS) Working Group from ISAS, Japan will launch a sounding rocket into low earth orbit to perform two activities: collect scientific information on the high power microwave-ionosphere interaction, and demonstrate microwave power transmission in space at 2.45 GHz. The SPS Working Group announced an open invitation to international agencies willing to collaborate with the Microwave Energy Transmission in Space (METS) experiment in a number of categories. Under the sponsorship of the NASA's Lewis Research Center, the Center for Space Power located at Texas A&M University joined the experiment by producing a microwave rectifying receiving antenna (rectenna). The rectenna is a special type of receiving antenna with unique properties and characteristics. The rectenna's main purpose is to efficiently convert microwave power into DC power. The rectenna is an advanced component in microwave power beaming technology developed for 2.45 GHz. The state-of-the-art rectenna for this frequency consists of dipole antennas, filter circuits, and transmission lines etched on a thin layer of Kapton film. The format of the thin film rectenna is ideally suited for space applications. Thin film rectennas have a low specific mass of approximately 1 kg/kW. The main component of the rectenna is the rectifying diode. High conversion efficiencies (90 percent) in microwave to DC power are capable with special Schottky barrier diodes correctly located in the rectenna circuitry. The theory of operation of the 2.45 GHz rectenna is explained. Experimental test results on the METS rectenna are presented. The packaging of the rectenna is also discussed to meet space qualifications.
Document ID
19940006885
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Brown, Alan M.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Subject Category
Communications And Radar
Report/Patent Number
NAS 1.26:193310
NASA-CR-193310
Report Number: NAS 1.26:193310
Report Number: NASA-CR-193310
Accession Number
94N11357
Funding Number(s)
CONTRACT_GRANT: NAG3-1368
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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