Velocity requirements, trip times, and initial mass in Earth-orbit requirements associated with round-trip Mars stopover missions that employ Venus swingby technique are summarized; results are compared with characteristics of standard opposition-class missions for every launch opportunity between 1980 and 1999; paper summarizes salient features of each mission and contains information useful in further studies relating to missions; it is also shown that single system design can be used efficiently to meet requirements for several mission opportunities.


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    Titel :

    Systematic comparison of Venus swingby mode with standard mode of mars round trips


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Deerwester, J.M. (Autor:in) / D'Haem, S.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    8 pages


    Medientyp :

    Standard


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :