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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    Titel :

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


    Beteiligte:
    J. M. Mansfield (Autor:in) / F. G. Etheridge (Autor:in) / J. Indrikis (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    96 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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