Analysis of trajectory constraints imposed on interplanetary mission launches from established parking orbit plane is presented; three major Earth-escape modes are defined and compared with respect to energy and plane-change requirements; single equation is developed which determines plane-change requirement for any mission in terms of parameters that cause it; example interplanetary missions to Venus and Mars are used to illustrate decrease in launching opportunity resulting from plane-change considerations.


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    Titel :

    Earth-departure plane change and launch window considerations for interplanetary missions


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    McLaughlin, J.F. (Autor:in) / Deerwester, J.M. (Autor:in) / Wolfe, J.F. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Earth-departure plane change and launch window considerations for interplanetary missions.

    DEERWESTER, J. M. / MCLAUGHLIN, J. F. / WOLFE, J. F. | AIAA | 1966


    Radiation Considerations for Interplanetary Missions

    United States; National Aeronautics and Space Administration / United States; Air Force / University of Houston-Clear Lake | British Library Conference Proceedings | 1992




    Analysis of Launch and Earth Departure Architectures for Near-Term Human Mars Missions

    Hofstetter, Wilfried / Guest, Arthur / McLinko, Ryan et al. | AIAA | 2008