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WRAP-RIB antenna technology developmentThe wrap-rib deployable antenna concept development is based on a combination of hardware development and testing along with extensive supporting analysis. The proof-of-concept hardware models are large in size so they will address the same basic problems associated with the design fabrication, assembly and test as the full-scale systems which were selected to be 100 meters at the beginning of the program. The hardware evaluation program consists of functional performance tests, design verification tests and analytical model verification tests. Functional testing consists of kinematic deployment, mesh management and verification of mechanical packaging efficiencies. Design verification consists of rib contour precision measurement, rib cross-section variation evaluation, rib materials characterizations and manufacturing imperfections assessment. Analytical model verification and refinement include mesh stiffness measurement, rib static and dynamic testing, mass measurement, and rib cross-section characterization. This concept was considered for a number of potential applications that include mobile communications, VLBI, and aircraft surveillance. In fact, baseline system configurations were developed by JPL, using the appropriate wrap-rib antenna, for all three classes of applications.
Document ID
19850015513
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Freeland, R. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Garcia, N. F.
(Lockheed Missiles and Space Co. Sunnyvale, Calif., United States)
Iwamoto, H.
(Lockheed Missiles and Space Co. Sunnyvale, Calif., United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1985
Publication Information
Publication: NASA. Langley Research Center Large Space Antenna Systems Technol., 1984
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
85N23824
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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