Linearization of equations of motion in curvilinear system of coordinates is described whose origin also moves at orbital rate on circular reference orbit; resulting equations can be used to study larger class of problems; to illustrate one of many ways these relations may be used in preliminary design, lunar launch and ascent phase of lunar orbit rendezvous mission is considered.


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    Titel :

    Study of certain aspects of lunar ascent and rendezvous with orbiting vehicle


    Weitere Titelangaben:

    AIAA -- Tech Papers


    Beteiligte:
    Burri, H.U. (Autor:in)

    Kongress:

    Meeting of the 2nd AIAA -- Manned Space Flight ; 1963 Rendezvous



    Erscheinungsdatum :

    1963


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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