Promising missions, selected on basis of minimum gross weight in Earth orbit, are available with long-duration class transfers (800 to 1000 days) during entire period investigated but are restricted to 1980's if short-duration (360 to 600 day) missions are desired; concept of multimission vehicle design is developed, and vehicle's capability is determined for several synodic periods; vehicle, with constant structural weight and tank size is capable of performing round-trip missions of various durations during several synodic periods.


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    Titel :

    Mars round-trip mission analysis for 1975-1985 time period


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Lascody, D.N. (Autor:in) / Thorson, E.D. (Autor:in) / Hawthorne, H.W. (Autor:in) / Markus, G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Mars round-trip mission analysis for the 1975- 1985 time period.

    Hawthorne, H. W. / Lascody, D. N. / Markus, G. et al. | NTRS | 1965


    Mars round-trip mission analysis for the 1975- 1985 time period

    HAWTHORNE, H. W. / LASCODY, D. N. / MARKUS, G. et al. | AIAA | 1965


    Mars round trip mission analysis for the unfavorable 1975-1985 time period

    HAWTHORNE, H. / LASCODY, D. / MARKUS, G. | AIAA | 1964


    Mars round trip mission analysis for the unfavorable 1975-1985 time period

    Hawthorne, H. W. / Lascody, D. N. / Markus, G. et al. | NTRS | 1964


    Round-Trip Mars Mission Mass Challenges

    L. M. Burke / M. A. Rucker / P. R. Chai et al. | NTIS | 2024