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contributor authorC.-Y. Lai
contributor authorZ. You
contributor authorS. Pellegrino
date accessioned2017-05-08T21:15:57Z
date available2017-05-08T21:15:57Z
date copyrightJuly 1998
date issued1998
identifier other%28asce%290893-1321%281998%2911%3A3%2873%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44877
description abstractThe shape and stress distribution in the new Collapsible Rib-Tensioned Surface reflector are investigated both analytically and experimentally. A methodology is established for the preliminary design of symmetric reflectors of given aperture, focal length, and target root-mean-square (RMS) error, by extending form-finding methods originally developed for membrane roof covers. The concepts of a reference surface and of an equilibrium surface are introduced, and algorithms are developed to compute these surfaces and their associated RMS error. Then, the cutting pattern for making the membrane is computed and the RMS error of the actual surface is predicted. Estimates are made of the RMS error of reflectors with apertures of 1, 3, 5, and 10 m, with 6, 12, and 24 ribs. Measurements of prestress and shape in a one-sixth sector of a 1 m diameter reflector with 6 ribs are compared with predictions obtained from the computational study. In the central part of the gore, about half of the total surface, the average error on prestress is 22% whereas the shape has an RMS error of 0.7 mm, better than predicted.
publisherAmerican Society of Civil Engineers
titleShape of Deployable Membrane Reflectors
typeJournal Paper
journal volume11
journal issue3
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(1998)11:3(73)
treeJournal of Aerospace Engineering:;1998:;Volume ( 011 ):;issue: 003
contenttypeFulltext


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