The high-performance, scalability and miniaturization requirements together with the power, mass and cost constraints mandate the use of commercial-off-the-shelf (COTS) components and standards in the X2000 avionics system architecture for deep-space missions.


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    Title :

    The Design of a Fault-Tolerant COTS-Based Bus Architecture For Space Applications


    Contributors:
    Tai, A. (author) / Alkalai, L. (author) / Chau, S. (author)

    Publication date :

    1999-06-15


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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