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Numerical analyses for the accurate design of large satellite on-board antennas

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Computational Mechanics ’95

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Abstract

This paper outlines three numerical analytical methods developed to design large deployable space antenna reflectors for advanced satellite communication. Considering the requirements that the reflectors must be large, deployable, accurate and light weight, metallic mesh reflector surfaces shaped by a cable network and a deployable truss are the best concept. [1].

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References

  1. J. Mitsugi and T. Yasaka: Proceedings of 17th Int. Sym. on Space Technology and Science, Vol.1, pp.599–604, 1991.

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Author information

Authors and Affiliations

  1. NTT Wireless Systems Laboratories, Yokosuka, Japan

    Kazuhide Ando & Jin Mitsugi

Authors
  1. Kazuhide Ando
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  2. Jin Mitsugi
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Editor information

Editors and Affiliations

  1. Computational Modeling Center, Georgia Institute of Technology, Atlanta, GA, 30332-0356, USA

    S. N. Atluri

  2. Department of Quantum Engineering & Systems Science, The University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113, Japan

    G. Yagawa

  3. Department of Mechanical Engineering, Vanderbilt University, P.O. Box 1592, Station B, Nashville, TN, 37235, USA

    Thomas Cruse

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© 1995 Springer-Verlag Berlin Heidelberg

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Ando, K., Mitsugi, J. (1995). Numerical analyses for the accurate design of large satellite on-board antennas. In: Atluri, S.N., Yagawa, G., Cruse, T. (eds) Computational Mechanics ’95. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-79654-8_49

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  • DOI: https://doi.org/10.1007/978-3-642-79654-8_49

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-79656-2

  • Online ISBN: 978-3-642-79654-8

  • eBook Packages: Springer Book Archive

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