As of late-July 2011, the ARTEMIS mission is transferring two spacecraft from Lissajous orbits around Earth-Moon Lagrange Point #1 into highly-eccentric lunar science orbits. This paper presents the trajectory design for the transfer from Lissajous orbit to lunar orbit insertion, the period reduction maneuvers, and the science orbits through 2013. The design accommodates large perturbations from Earth's gravity and restrictive spacecraft capabilities to enable opportunities for a range of heliophysics and planetary science measurements. The process used to design the highly-eccentric ARTEMIS science orbits is outlined. The approach may inform the design of future planetary moon missions.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    ARTEMIS Lunar Orbit Insertion and Science Orbit Design Through 2013


    Beteiligte:

    Kongress:

    AAS/AIAA Astrodynamics Specialist Conference ; 2011 ; Girdwood, AK, United States


    Erscheinungsdatum :

    2015-01-01


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch




    ARTEMIS Lunar Orbit Insertion and Science Orbit Design Through 2013

    Broschart, Stephen B. / Sweetser, Theodore H. / Angelopoulos, Vassilis et al. | NTRS | 2011


    ARTEMIS Lunar Orbit Insertion and Science Orbit Design Through 2013 (AAS 11-509)

    Broschart, S.B. / Sweetser, T.H. / Angelopoulos, V. et al. | British Library Conference Proceedings | 2012


    GRAIL Trajectory Design: Lunar Orbit Insertion through Science

    Hatch, S. / Roncoli, R. / Sweetser, T. et al. | British Library Conference Proceedings | 2010


    GRAIL Trajectory Design: Lunar Orbit Insertion through Science

    Hatch, Sara / Roncoli, Ralph / Sweetser, Theodore | AIAA | 2010


    Orbit Determination of Hiten for Insertion into Lunar Orbit

    Miller, James K. / Efron, Leonard / Menon, Premkumar R. | NTRS | 1993