Examination of requirements for multiman crew transport and operational disadvantages of lunar orbital mission mode; possibilities for landing multiman crews in direct mission mode, booster system requirements and state of art in necessary subsystems; possible evolutionary program which uses extensions of present programs and new developments is shown; concepts which seem to have merits such as extended Apollo/LOR modification which could increase landed crew by 50%, or one man (three vs present two); however, substantial logistic cargo landing capability may be required; one- or two-stage service module landers would be adaptable to service, providing 20,000-lb of cargo landed per Saturn V launch.


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    Titel :

    Next-generation lunar transports


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:

    Kongress:

    SAE Meeting ; 1966 Lunar



    Erscheinungsdatum :

    1966


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Next-Generation Lunar Transports

    Matzenauer, J. O. | SAE Technical Papers | 1966


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    The GTCP331 Auxiliary Power Unit for the Next Generation Commercial Transports

    Romanin, Aldo L. / Wells, Robert E. | SAE Technical Papers | 1980