Electrical power for the MUSES-C scientific satellite is provided by deployable solar array wings. The solar array is a small rigid panel type and the wings can provide more than 2.57 kW at EOL, using advanced solar cells. The flight model of the MUSES-C solar array has been built and the wing acceptance test is underway. This paper presents the electrical and mechanical design and the prototype wing tests results of MUSES-C solar array.


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    Title :

    Muses-C solar array electrical and mechanical design


    Additional title:

    Elektrischer und mechanischer Entwurf des Sonnenzellenflügels von MUSES-C


    Contributors:
    Takahashi, K. (author) / Okada, Y. (author) / Arai, H. (author) / Tajima, M. (author) / Higuchi, K. (author)


    Publication date :

    2002


    Size :

    6 Seiten, 12 Bilder, 6 Tabellen




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    MUSES-C Solar Array Electrical and Mechanical Design

    Takahashi, K. / Okada, Y. / Arai, H. et al. | British Library Conference Proceedings | 2002


    Development of Muses-B Solar Array

    Shibayama, Y. / Takahashi, J. / Onoda, J. et al. | British Library Conference Proceedings | 1995


    Development of Muses-B Solar Array

    Shibayama, Y. / Takahashi, J. / Onoda, J. et al. | British Library Online Contents | 1995


    MUSES-A

    Nishimura, T. / Hayashi, T. | NTRS | 1991


    MUSES-A

    T. Nishimura / T. Hayashi | NTIS | 1991