The firing of a fixed impulse spin stabilized upper stage following shuttle deployment of a geosynchronous payload was examined in detail. Design of the transfer trajectory was discussed in terms of finding both a nominal and possible dispersion case that can be handled operationally within the allotted trim fuel budget.


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    Titel :

    Transfer trajectory design for a shuttle launched geosynchronous payload


    Beteiligte:
    Defazio, R. L. (Autor:in)


    Erscheinungsdatum :

    01.04.1979


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



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