Structural design of ultra-lightweight spin axis extendable mast using inflation extension method

Kazuki Watanabe, Ken Higuchi, Akihito Watanabe, Hiroaki Tsunoda, Hiroshi Yamakawa, Tadahiko Sekiya

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

    Abstract

    Inflatable structure is a promising technology with low weight, ease of packaging and reliability. Space inflatable antenna rod (SPINAR) has been developed as an ultra-light one-dimensional extendible structure driven by an inflatable actuator. SPINAR satisfies ever-intensifying requirements such as lightweight, high rigidity, high strength, high packaging efficiency, favorable antenna performance and simple extension mechanisms. For a scientific mission under consideration in ISAS/JAXA, the analysis of the requirements for structural design of one-dimensional extendible antenna structure and the detailed conceptual design were performed. Also, the spin extension test of SPINAR on a turntable under micro-gravity environment using airplane parabolic flight was conducted. In this paper, the analysis and evaluation of the structural feature and system performance are discussed based on the manufacturing the experimental model and the micro-gravity test.

    Original languageEnglish
    Title of host publicationInternational Astronautical Federation - 56th International Astronautical Congress 2005
    Pages3486-3493
    Number of pages8
    Volume5
    Publication statusPublished - 2005
    EventInternational Astronautical Federation - 56th International Astronautical Congress 2005 - Fukuoka
    Duration: 2005 Oct 172005 Oct 21

    Other

    OtherInternational Astronautical Federation - 56th International Astronautical Congress 2005
    CityFukuoka
    Period05/10/1705/10/21

    Fingerprint

    structural design
    Structural design
    inflation
    antenna
    antennas
    Antennas
    rods
    Microgravity
    microgravity
    packaging
    Packaging
    inflatable structures
    Inflatable structures
    parabolic flight
    gravity
    Phonographs
    low weight
    requirements
    rigidity
    Conceptual design

    ASJC Scopus subject areas

    • Space and Planetary Science
    • Aerospace Engineering

    Cite this

    Watanabe, K., Higuchi, K., Watanabe, A., Tsunoda, H., Yamakawa, H., & Sekiya, T. (2005). Structural design of ultra-lightweight spin axis extendable mast using inflation extension method. In International Astronautical Federation - 56th International Astronautical Congress 2005 (Vol. 5, pp. 3486-3493)

    Structural design of ultra-lightweight spin axis extendable mast using inflation extension method. / Watanabe, Kazuki; Higuchi, Ken; Watanabe, Akihito; Tsunoda, Hiroaki; Yamakawa, Hiroshi; Sekiya, Tadahiko.

    International Astronautical Federation - 56th International Astronautical Congress 2005. Vol. 5 2005. p. 3486-3493.

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

    Watanabe, K, Higuchi, K, Watanabe, A, Tsunoda, H, Yamakawa, H & Sekiya, T 2005, Structural design of ultra-lightweight spin axis extendable mast using inflation extension method. in International Astronautical Federation - 56th International Astronautical Congress 2005. vol. 5, pp. 3486-3493, International Astronautical Federation - 56th International Astronautical Congress 2005, Fukuoka, 05/10/17.
    Watanabe K, Higuchi K, Watanabe A, Tsunoda H, Yamakawa H, Sekiya T. Structural design of ultra-lightweight spin axis extendable mast using inflation extension method. In International Astronautical Federation - 56th International Astronautical Congress 2005. Vol. 5. 2005. p. 3486-3493
    Watanabe, Kazuki ; Higuchi, Ken ; Watanabe, Akihito ; Tsunoda, Hiroaki ; Yamakawa, Hiroshi ; Sekiya, Tadahiko. / Structural design of ultra-lightweight spin axis extendable mast using inflation extension method. International Astronautical Federation - 56th International Astronautical Congress 2005. Vol. 5 2005. pp. 3486-3493
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