Stepwise deployment of membrane structures with rolled-up booms

Experiments and simulations

Nobukatsu Okuizumi, Nobuhisa Katsumata, Hiroaki Kobayashi, Hiroyuki Ikuta, Masakazu Yamazaki, Yuki Ito, M. C. Natori, Hiroshi Yamakawa

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    4 Citations (Scopus)

    Abstract

    In this paper, simple deployable structures are introduced, which consist of polygonal membranes and elastic booms deployed by only releasing the rolled-up booms in stepwise manners. The membranes are folded up with modified spiral folding patterns to fit the arrangement of booms. The booms are newly-developed bi-convex tapes covered by braids. Basic mechanical test results of the booms are first presented. Deployment experiments of a small conceptual model are demonstrated for several configurations. Numerical simulations of the deployment experiments are also performed employing multi-particle approximation method for membranes and a discrete model for one-dimensional continuum for the booms. The results are compared with the experimental results and the deployment behaviors of the structures are discussed.

    Original languageEnglish
    Title of host publicationAIAA Spacecraft Structures Conference
    DOIs
    Publication statusPublished - 2014
    EventAIAA Spacecraft Structures Conference - SciTech Forum and Exposition 2014 - National Harbor, MD
    Duration: 2014 Jan 132014 Jan 17

    Other

    OtherAIAA Spacecraft Structures Conference - SciTech Forum and Exposition 2014
    CityNational Harbor, MD
    Period14/1/1314/1/17

    Fingerprint

    Membrane structures
    Membranes
    Experiments
    Tapes
    Computer simulation

    ASJC Scopus subject areas

    • Computer Science(all)
    • Aerospace Engineering
    • Electrical and Electronic Engineering
    • Mechanical Engineering

    Cite this

    Okuizumi, N., Katsumata, N., Kobayashi, H., Ikuta, H., Yamazaki, M., Ito, Y., ... Yamakawa, H. (2014). Stepwise deployment of membrane structures with rolled-up booms: Experiments and simulations. In AIAA Spacecraft Structures Conference https://doi.org/10.2514/6.2014-1039

    Stepwise deployment of membrane structures with rolled-up booms : Experiments and simulations. / Okuizumi, Nobukatsu; Katsumata, Nobuhisa; Kobayashi, Hiroaki; Ikuta, Hiroyuki; Yamazaki, Masakazu; Ito, Yuki; Natori, M. C.; Yamakawa, Hiroshi.

    AIAA Spacecraft Structures Conference. 2014.

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Okuizumi, N, Katsumata, N, Kobayashi, H, Ikuta, H, Yamazaki, M, Ito, Y, Natori, MC & Yamakawa, H 2014, Stepwise deployment of membrane structures with rolled-up booms: Experiments and simulations. in AIAA Spacecraft Structures Conference. AIAA Spacecraft Structures Conference - SciTech Forum and Exposition 2014, National Harbor, MD, 14/1/13. https://doi.org/10.2514/6.2014-1039
    Okuizumi N, Katsumata N, Kobayashi H, Ikuta H, Yamazaki M, Ito Y et al. Stepwise deployment of membrane structures with rolled-up booms: Experiments and simulations. In AIAA Spacecraft Structures Conference. 2014 https://doi.org/10.2514/6.2014-1039
    Okuizumi, Nobukatsu ; Katsumata, Nobuhisa ; Kobayashi, Hiroaki ; Ikuta, Hiroyuki ; Yamazaki, Masakazu ; Ito, Yuki ; Natori, M. C. ; Yamakawa, Hiroshi. / Stepwise deployment of membrane structures with rolled-up booms : Experiments and simulations. AIAA Spacecraft Structures Conference. 2014.
    @inproceedings{95a90dcaa91e4aefb53e8203320fcaaf,
    title = "Stepwise deployment of membrane structures with rolled-up booms: Experiments and simulations",
    abstract = "In this paper, simple deployable structures are introduced, which consist of polygonal membranes and elastic booms deployed by only releasing the rolled-up booms in stepwise manners. The membranes are folded up with modified spiral folding patterns to fit the arrangement of booms. The booms are newly-developed bi-convex tapes covered by braids. Basic mechanical test results of the booms are first presented. Deployment experiments of a small conceptual model are demonstrated for several configurations. Numerical simulations of the deployment experiments are also performed employing multi-particle approximation method for membranes and a discrete model for one-dimensional continuum for the booms. The results are compared with the experimental results and the deployment behaviors of the structures are discussed.",
    author = "Nobukatsu Okuizumi and Nobuhisa Katsumata and Hiroaki Kobayashi and Hiroyuki Ikuta and Masakazu Yamazaki and Yuki Ito and Natori, {M. C.} and Hiroshi Yamakawa",
    year = "2014",
    doi = "10.2514/6.2014-1039",
    language = "English",
    booktitle = "AIAA Spacecraft Structures Conference",

    }

    TY - GEN

    T1 - Stepwise deployment of membrane structures with rolled-up booms

    T2 - Experiments and simulations

    AU - Okuizumi, Nobukatsu

    AU - Katsumata, Nobuhisa

    AU - Kobayashi, Hiroaki

    AU - Ikuta, Hiroyuki

    AU - Yamazaki, Masakazu

    AU - Ito, Yuki

    AU - Natori, M. C.

    AU - Yamakawa, Hiroshi

    PY - 2014

    Y1 - 2014

    N2 - In this paper, simple deployable structures are introduced, which consist of polygonal membranes and elastic booms deployed by only releasing the rolled-up booms in stepwise manners. The membranes are folded up with modified spiral folding patterns to fit the arrangement of booms. The booms are newly-developed bi-convex tapes covered by braids. Basic mechanical test results of the booms are first presented. Deployment experiments of a small conceptual model are demonstrated for several configurations. Numerical simulations of the deployment experiments are also performed employing multi-particle approximation method for membranes and a discrete model for one-dimensional continuum for the booms. The results are compared with the experimental results and the deployment behaviors of the structures are discussed.

    AB - In this paper, simple deployable structures are introduced, which consist of polygonal membranes and elastic booms deployed by only releasing the rolled-up booms in stepwise manners. The membranes are folded up with modified spiral folding patterns to fit the arrangement of booms. The booms are newly-developed bi-convex tapes covered by braids. Basic mechanical test results of the booms are first presented. Deployment experiments of a small conceptual model are demonstrated for several configurations. Numerical simulations of the deployment experiments are also performed employing multi-particle approximation method for membranes and a discrete model for one-dimensional continuum for the booms. The results are compared with the experimental results and the deployment behaviors of the structures are discussed.

    UR - http://www.scopus.com/inward/record.url?scp=84894458023&partnerID=8YFLogxK

    UR - http://www.scopus.com/inward/citedby.url?scp=84894458023&partnerID=8YFLogxK

    U2 - 10.2514/6.2014-1039

    DO - 10.2514/6.2014-1039

    M3 - Conference contribution

    BT - AIAA Spacecraft Structures Conference

    ER -