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A new fabrication method for precision antenna reflectors for space flight and ground testThe use of higher frequencies on communications satellites has led to the requirement for increasingly precise antenna reflectors for use in space. Typical industry fabrication methods for space antenna reflectors employ successive molding techniques for reflector face sheets and a final fit-up to a master mold in order to achieve the required accuracies. However, new missions at much higher frequencies will require greater accuracies than may be achievable using these present methods. A new approach for the fabrication of ground-test antenna reflectors is to machine the reflective surface into a stainless steel and fiberglass composite structure. A 2.7-m diameter ground-test antenna reflector fabricated using this method has an accuracy of better than 0.013 mm (0.0005 in.) rms. A similar design concept for a solid surface reflector for use on spacecraft would involve fabrication in a similar manner but using space-qualified materials. This report describes the design, analysis, and fabrication of the 2.7-m-diameter precision antenna reflector for antenna ground test and the extension of this technology to precision space antenna reflectors.
Document ID
19900038572
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sharp, G. Richard
(NASA Lewis Research Center Cleveland, OH, United States)
Wanhainen, Joyce S.
(NASA Lewis Research Center Cleveland, OH, United States)
Ketelsen, Dean A.
(Arizona, University Tucson, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Communications And Radar
Report/Patent Number
AIAA PAPER 90-0803
Meeting Information
Meeting: AIAA International Communication Satellite Systems Conference and Exhibit
Location: Los Angeles, CA
Country: United States
Start Date: March 11, 1990
End Date: March 15, 1990
Accession Number
90A25627
Distribution Limits
Public
Copyright
Other

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