The feasibility of developing a solar electric multimission spacecraft (SEMMS) is examined with emphasis on understanding the effect of solar electric propulsion elements on a spacecraft system design. The applicability of Mariner, Viking, and thermoelectric outer planet spacecraft (TOPS) technologies to postulated mission/science objectives is investigated. A Mariner/Viking-based, modular spacecraft evolves which, with minimum modifications, is capable of performing a variety of interplanetary missions, including comet and asteroid rendezvous and orbit of Mercury, Jupiter, and Saturn. An early technology-evaluation flight is recommended to minimize the risk in subsequent missions.


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    Title :

    SEMMS - Understanding the solar electric multimission concept.


    Contributors:

    Conference:

    American Institute of Aeronautics and Astronautics, Electric Propulsion Conference ; 1972 ; Bethesda, MD


    Publication date :

    1972-04-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English