The modularity, shape, and size of the recommended platform concept offers a low investment, early option to demonstrate the system; flexibility to conservative growth; adaptability to great variety of multi or dedicated payload groups; and good dispersion and viewing freedom for payloads. Platform configuration effectively supports 80 to 85% of the NASA/OSS and OSTA payloads. The subsystem approaches recommended are based on cost effective distribution of functions.


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    Title :

    Conceptual design study. Science and Applications Space Platform (SASP). Final briefing


    Publication date :

    1980-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English