Technical feasibility is studied by Marshall Space Flight Center of sending manned reconnaissance flyby missions to Mars and Venus; 1975 Venus mission of 380 to 394 days and 1978 Mars mission of 661 to 691 days duration were investigated and vehicles and propulsion systems considered; manned Mars and Venus reconnaissance flyby missions appear feasible in mid and late 1970's assuming all chemical propulsion and using Saturn/Apollo hardware; missions require extensions to Saturn/Apollo technology state of art in following areas -- lifetime of astrionic systems, orbital operations/tanking, internal power-supply systems, and life-support system.


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    Titel :

    On practicality of manned planetary flyby missions


    Weitere Titelangaben:

    ASME -- Paper


    Beteiligte:
    Smith, J.N. (Autor:in)

    Kongress:

    ASME Meeting AV-9 ; 1965 Interplanetary



    Erscheinungsdatum :

    1965


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Analysis of planetary flyby missions

    Ragsac, R.V. / Titus, R.R. | Engineering Index Backfile | 1963


    A Venus lander probe for manned flyby missions

    Chandeysson, P. L. | NTRS | 1968


    A Venus Lander Probe for Manned Flyby Missions

    P. L. Chandeysson | NTIS | 1968