Model which optimizes long-term, continuous-operation missions performed by earth-orbiting space station; model is based on use of arbitrary cost-effectiveness criterion; space station operating time availability is shown as function of cost for arbitrary mission lengths and payloads; resupply vehicles are used to support separately-launched, "permanent" space station; critical reliability and maintainability problems; model was developed on basis of results obtained during detailed in-depth studies of actual systems; it was programmed for and run on high-speed digital computer.


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    Titel :

    Optimization of earth-orbiting space station missions


    Weitere Titelangaben:

    Reliability Maintainability Conference -- Proc


    Beteiligte:
    Hunt, G.C. (Autor:in) / Ridley, H. (Autor:in)

    Kongress:

    Proceedings of the 5th Reliability and Maintainability Conference ; 1966 Reliability



    Erscheinungsdatum :

    1966


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    TEiE OPTIMIZATION OF EARTH-ORBITING SPACE STATION MISSIONS

    HUNT, GORDON / RIDLEY, HOWARD | AIAA | 1966


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