Voyager concept covers orbiting and landing-capsule missions to planets, initially Mars; one possible Voyager concept is considered; spacecraft would consist of bus, propulsion unit, and landing capsule; for orbiting missions propulsion unit would place bus into planetary orbit; Saturn IB/Centaur launch vehicle may be used for Voyager; launch energy requirements and series of Mars missions from 1971 to 1977; characteristics and potential technical problem areas of each module.


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    Title :

    Voyager


    Additional title:

    Astronautics Aeronautics


    Contributors:

    Published in:

    Publication date :

    1965


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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