ARTEMIS (Acceleration, Reconnection, Turbulence and Electrodynamics of the Moon's Interaction with the Sun) repurposed two spacecraft to extend their useful science (Angelopoulos, 2010) by moving them via lunar gravity assists from elliptical Earth orbits to L1 and L2 Earth-Moon libration orbits and then to lunar orbits by exploiting the Earth-Moon-Sun dynamical environment. This paper describes the complete design from conceptual plans using weak stability transfer options and lunar gravity assist to the implementation and operational support of the Earth-Moon libration and lunar orbits. The two spacecraft of the ARTEMIS mission will have just entered lunar orbit at this paper's presentation.


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    Titel :

    ARTEMIS Mission Overview: From Concept to Operations


    Beteiligte:
    Folta, David (Autor:in) / Sweetser, Theodore (Autor:in)

    Kongress:

    American Astronautical Society/American Institute of Aeronautics and Astronautics (AAS/AIAA) Astrodynamics Specialist Conference ; 2011 ; Girdwood, AK, United States


    Erscheinungsdatum :

    2011-07-31


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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