It is pointed out that if the difference between the nodal crossing time of the Shuttle parking orbit and the final orbit of a spacecraft is more than about half an hour, current design spacecraft may have to carry a prohibitively large propulsion system to meet its requirements. Various solutions to this problem are discussed.


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    Titel :

    Multiple payload Shuttle flights from WTR - Some operational and orbital mechanics considerations


    Beteiligte:
    Edgecombe, D. S. (Autor:in) / Fischer, N. H. (Autor:in) / Rea, F. G. (Autor:in)

    Kongress:

    International Astronautical Congress


    Erscheinungsdatum :

    1981-09-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :