2012
DOI: 10.1088/0964-1726/21/7/075013
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Deployable auxetic shape memory alloy cellular antenna demonstrator: design, manufacturing and modal testing

Abstract: This work describes the design, manufacturing and testing of a deployable antenna for deep-space missions based on a hybrid honeycomb truss made of shape memory alloy (SMA). The deployable characteristics are enhanced by the equivalent auxetic (negative Poisson’s ratio) behaviour of the cellular configuration. Specific emphasis is placed on the modal analysis techniques used to test the lightweight SMA structure.

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Cited by 77 publications
(52 citation statements)
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“…Auxetic materials, i.e. materials, which expand laterally when a uniaxial load is applied, have received a significant amount of interest in the past few decades . Auxetic character is known to be a scale independent characteristic , being the product of particular geometries undergoing a specific deformation mechanism.…”
Section: Introductionmentioning
confidence: 99%
“…Auxetic materials, i.e. materials, which expand laterally when a uniaxial load is applied, have received a significant amount of interest in the past few decades . Auxetic character is known to be a scale independent characteristic , being the product of particular geometries undergoing a specific deformation mechanism.…”
Section: Introductionmentioning
confidence: 99%
“…Other works about the development of honeycombs and cellular structures with different types of SMA materials and geometry can be found in [38][39][40][41]. A shape memory alloy cellular structure that exploits the auxetic nature of the chiral configuration has been also developed to create a deployable demonstrator [42] and space antenna [43]. Rossiter et al [44] have also produced a deployable chiral honeycomb, this time using SMP (CRG Veriflex laminate) to achieve greater deployment strains and lower density and metastable configurations.…”
Section: Introductionmentioning
confidence: 99%
“…The penalty that shall be paid for the related efficiency reduction (1 to 5) is well compensated by the decrease in the number of pieces (a good index for reliability and maintenance), weight savings, and compactness. This advantage can be also exploited for other on-board components like landing gears, deployable antennas and others [22][23][24][25][26][27][28][29][30][31].…”
Section: Introductionmentioning
confidence: 99%