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Deployment simulations of inflatable tensegrity structures
KTH, School of Engineering Sciences (SCI), Mechanics, Structural Mechanics.
KTH, School of Engineering Sciences (SCI), Mechanics, Structural Mechanics.ORCID iD: 0000-0001-6802-8331
2008 (English)In: International Journal of Space Structures, ISSN 0956-0599, Vol. 23, no 2, 63-77 p.Article in journal (Refereed) Published
Abstract [en]

nsegrity structures are attractive as deployable space structures since they are composed mainly of flexible tension members and can thus easily be folded. To automatically deploy such structures it is proposed that the tension members are replaced or enclosed by thin-film tubes, which form a continuous volume. The structure deploys when this volume is pressurised. This concept was studied by numerical simulations of the deployment process in a zero-gravity environment using the control volume method for the fluid-structure interaction. First, single z-folded and coiled tubes were analysed to determine suitable element size, number of control volumes and gas flow rate. Then one- and three-stage tensegrity masts were modelled, folded and finally deployed. The study showed that the deployment concept is feasible.

Place, publisher, year, edition, pages
Multi-Science Publishing, 2008. Vol. 23, no 2, 63-77 p.
Keyword [en]
Control volume, Deployment, Inflatable structures, Tensegrity
National Category
Applied Mechanics
Identifiers
URN: urn:nbn:se:kth:diva-83150DOI: 10.1260/026635108785260597Scopus ID: 2-s2.0-49749130036OAI: oai:DiVA.org:kth-83150DiVA: diva2:498747
Note
QC 20120213Available from: 2012-02-12 Created: 2012-02-12 Last updated: 2017-12-07Bibliographically approved

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Publisher's full textScopushttp://multi-science.metapress.com/content/c1n5772kh5814w10/

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Tibert, Gunnar

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