Eight deployable platform design objectives were established: autodeploy/retract; fully integrated utilities; configuration variability; versatile payload and subsystem interfaces; structural and packing efficiency; 1986 technology readiness; minimum EVA/RMS; and Shuttle operational compatibility.


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    Title :

    Development of deployable structures for large space platform systems, part 1


    Contributors:
    Cox, R. L. (author) / Nelson, R. A. (author)

    Publication date :

    1982-10-25


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English