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. TAS4.4: Concept Design


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

    Erscheinungsdatum :

    1976


    Format / Umfang :

    94 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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