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Five meter diameter conical furlable antennaAn investigation was made to demonstrate that a 5-meter-diameter, furlable, conical reflector antenna utilizing a line source feed can be fabricated utilizing composite materials and to prove that the antenna can function mechanically and electrically as prototype flight hardware. The design, analysis, and testing of the antenna are described. An RF efficiency of 55% at 8.5 GHz and a surface error of 0.64 mm rms were chosen as basic design requirements. Actual test measurements yielded an efficiency of 53% (49.77 dB gain) and a surface error of 0.61 mm rms. Atmospherically induced corrosion of the reflector mesh resulted in the RF performance degradation. An assessment of the antenna as compared to the current state of the art technology was made. This assessment included cost, surface accuracy and RF performance, structural and mechanical characteristics, and possible applications.
Document ID
19760020391
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Fortenberry, J. W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Freeland, R. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Moore, D. M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 3, 2013
Publication Date
July 15, 1976
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
JPL-TR-32-1604
NASA-CR-148457
Report Number: JPL-TR-32-1604
Report Number: NASA-CR-148457
Accession Number
76N27479
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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