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Analytical performance prediction for large antennasA linear mathematical modeling of the static and dynamic characteristics of a deployable offset wrap rib antenna was attempted using small motions in an effort to simulate the surface distortion resulting from thermal loading and transient oscillations from control. Both cyclic symmetry and model synthesis were used for parametric analysis. Although the ribs can be modeled as slender beams varying cross sections and equivalent linear material properties, the mesh poses a problem since its equivalent stress strain relations are highly nonlinear and sensitive to the biaxial prestressed state. Consequently, the macroscopic material properties were measured experimentally in the neighborhood of the design prestress. An equivalent tangent modulus technique was then adopted about this equilibrium state and assumed to be valid within a small range of incremental stresses.
Document ID
19810010661
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
El-Raheb, M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 11, 2013
Publication Date
February 1, 1981
Publication Information
Publication: NASA. Langley Research Center Large Space Systems Technol., 1980, Vol. 1
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
81N19188
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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