For some three decades, the Apollo-style mission has served as a proven baseline technique for transporting flight crews to the Moon and back with expendable hardware. This approach provides an optimal design for expeditionary missions, emphasizing operational flexibility in terms of safely returning the crew in the event of a hardware failure. However, its application is limited essentially to low-latitude lunar sites, and it leaves much to be desired as a model for exploratory and evolutionary programs that employ reusable space-based hardware. This study compares the performance requirements for a lunar orbit rendezvous mission type with one using the cislunar libration point (L1) as a stopover and staging point for access to arbitrary sites on the lunar surface. For selected constraints and mission objectives, it contrasts the relative uniformity of performance cost when the L1 staging point is used with the wide variation of cost for the Apollo-style lunar orbit rendezvous.


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    Title :

    Earth to Moon Transfer: Direct vs Via Libration Points (L1, L2)


    Contributors:

    Conference:

    27th annual AAS Guidance and Control Conference ; 2004 ; Breckenridge, CO, United States


    Publication date :

    2004-02-04


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English






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