The application of forces in multi-body dynamical environments to permit the transfer of spacecraft from Earth orbit to Sun-Earth weak stability regions and then return to the Earth-Moon libration (L1 and L2) orbits has been successfully accomplished for the first time. This demonstrated that transfer is a positive step in the realization of a design process that can be used to transfer spacecraft with minimal Delta-V expenditures. Initialized using gravity assists to overcome fuel constraints; the ARTEMIS trajectory design has successfully placed two spacecrafts into Earth-Moon libration orbits by means of these applications.


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    Titel :

    Applications of Multi-body Dynamical Environments: The ARTEMIS Transfer Trajectory Design


    Beteiligte:
    Folta, David C. (Autor:in) / Woodard, Mark (Autor:in) / Howell, Kathleen (Autor:in) / Patterson, Chris (Autor:in) / Schlei, Wayne (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2011-12-23



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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