Titlebook: IUTAM-IASS Symposium on Deployable Structures: Theory and Applications; Proceedings of the I S. Pellegrino,S. D. Guest Conference proceedin

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Inflatable Tensioned Membrane Waveguide Antenna Array for Space Applications,olving small spacecraft. Examples of these mission applications include microwave communications, synthetic aperture radar (SAR) and Earth Science remote sensing; as well as inter-planetary missions such as very long baseline interferometry. Many of these missions require the use of large aperture a

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Wing Folding in Beetles,on it is imperative that their delicate membranes can be safely stowed away when not in use. Dragonflies are one of the few groups to rest with the wings fully outstretched, the others having a basal hinge that allows the wings to be drawn automatically towards the body when they stop flying. Detail

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Symmetry as a Basis for Morphological Analysis and Generation of NASA-Type Cubic Deployables,analysis and modeling of several of NASA’s deployable truss structures by Alan Britt in 1997 in our Morphology Studio. In late 1997 we undertook to define a morphological method of generating deployable structures, based on crystallographic symmetry. Having modeled and developed variants for three N

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Intercept

Design, Construction and Testing of the Deployable UHF Antenna for Skynet 4 Stage 2,ced version of the Stage 1 satellites with tuneable UHF, increased UHF transponder power, and new Earth-cover helical UHF antenna designed and built by AEA Technology. The contract for the supply of the flight UHF antennas was awarded following the successful testing of the Qualification Model anten

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Foldable Rigid Connections,owever, for terrestrial structures subjected to the gravity load, wind load or inertia force due to earthquakes, moment frames consisting of beams, columns and connections with bending moment rigidity are often constructed. In the paper a key idea is proposed to make such moment frames foldable. A s