Enable future missions Any mission to a DRO or halo orbit could benefit from the capability to transfer between these orbits Chemical propulsion could be used for these transfers, but at high propellant cost Fill gaps in knowledge A variety of transfers using SEP or solar sails have been studied for the Earth-Moon system Most results in literature study a single transfer This is a step toward understanding the wide array of types of transfers available in an N-body force model.


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    Title :

    Low-Thrust Transfers from Distant Retrograde Orbits to L2 Halo Orbits in the Earth-Moon System


    Contributors:
    N. L. Parrish (author) / J. S. Parker (author) / S. P. Hughes (author) / J. Heiligers (author)

    Publication date :

    2016


    Size :

    25 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Low-Thrust Transfers from Distant Retrograde Orbits to L2 Halo Orbits in the Earth-Moon System

    Parrish, Nathan L. / Parker, Jeffrey S. / Hughes, Steven P. et al. | NTRS | 2016


    Low-Thrust Transfers from Distant Retrograde Orbits to L2 Halo Orbits in the Earth-Moon System

    Parrish, Nathan L. / Parker, Jeffrey S. / Hughes, Steven P. et al. | NTRS | 2016



    Transfers to Earth-Moon L3 Halo Orbits

    Davis, Kathryn / Born, George / Deilami, Masoud et al. | AIAA | 2012


    Transfers to Earth–Moon L3 halo orbits

    Davis, Kathryn | Online Contents | 2013