Evaluations are presented of alternative LANDSAT follow-on launch configurations to derive the propulsion requirements for the multimission modular spacecraft (MMS). Two basic types were analyzed including use of conventional launch vehicles and shuttle-supported missions. It was concluded that two sizes of modular hydrazine propulsion modules would provide the most cost-effective combination for future missions of this spacecraft. Conceptual designs of the selected propulsion modules were performed to the depth permitting determination of mass properties and estimated costs.


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    Title :

    Landsat/MMS Propulsion Module Design. Volume 1: Task 4.3, Trade Studies


    Contributors:

    Publication date :

    1976


    Size :

    96 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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