The design, capabilities, and subsystem options are described for the Boeing Small Research Module (BSRM). Specific scientific missions are defined and the BSRM capability to support these missions is discussed. Launch vehicle integration requirements and spacecraft operational features are also presented.


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    Title :

    Feasibility study of the Boeing Small Research Module (BSRM) concept


    Publication date :

    1975-03-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English