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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    Title :

    Optimization of earth-orbiting space station missions


    Additional title:

    Reliability Maintainability Conference -- Proc


    Contributors:
    Hunt, G.C. (author) / Ridley, H. (author)

    Conference:

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



    Publication date :

    1966


    Size :

    9 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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