The primary objective of this study was to determine the shape and weight of an STP Standard Satellite which would have a maximum probability of being launched 'piggy-back' on an STS mission between 1980-1990. The study was conducted in two parts. Part 1 consisted of two tasks, Mission Analysis and System Analysis. In these tasks, a shuttle mission model was selected, preliminary STP-STD-satellite capabilities defined and each shuttle mission examined to determine the excess volume and weight available.


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    Titel :

    Space Test Program Standard Satellite Launch Optimization Study


    Beteiligte:
    M. A. Cantor (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    122 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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