This paper presents a proof of concept an feasibility assessment of such a system, demonstrating 38% cost savings for a baseline mission.


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    Title :

    Low Earth orbit constellation design using the Earth-Moon L1 point


    Contributors:
    Kasdin, N. J. (author) / Gralla, Erica (author) / Chow, Naomi (author)

    Publication date :

    2004-02-01


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English



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