No AccessDeployment Dynamics of Self-deployable Truss Structure Consisting of Bi-convex BoomsAkihiro Tamura, Shota Inoue, Daishi Kawarabayashi, Masahiko Yamazaki and Yasuyuki MiyazakiAkihiro TamuraNihon UniversitySearch for more papers by this author, Shota InoueNihon UniversitySearch for more papers by this author, Daishi KawarabayashiNihon UniversitySearch for more papers by this author, Masahiko YamazakiNihon UniversitySearch for more papers by this author and Yasuyuki MiyazakiNihon UniversitySearch for more papers by this authorAIAA 2017-0175Session: Deployable Booms and FlexuresPublished Online:5 Jan 2017https://doi.org/10.2514/6.2017-0175SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited bySystem Design, Development and Ground Verification of a Separable De-Orbit Mechanism for the Orbital Manoeuvre of Micro-Satellite ALE-11 Jan 2021 | TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, Vol. 19, No. 3Membrane Structure Supported by Self-Deployable Truss for Space ApplicationsYasuyuki Miyazaki, Momoko Fukunaga and Daiki Kousaka7 January 2018 What's Popular 4th AIAA Spacecraft Structures Conference 9 - 13 January 2017Grapevine, Texashttps://doi.org/10.2514/6.2017-0175 CrossmarkInformationCopyright © 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. TopicsAerospace SciencesAstronauticsComputational Fluid DynamicsFlexible and Active StructuresFluid DynamicsNumerical AnalysisStructural EngineeringStructural SystemStructures, Design and TestTrusses KeywordsTrussesMicro GravityKinetic EnergyPoisson's RatioLarge Space StructuresAeroplaneNumerical AnalysisAeronauticsSolar SailStructural MembersDigital Topics Spacecraft Structures