The Dawn Project's mission is to rendezvous and map the two heaviest main belt asteroids Vesta and Ceres. The Ion Propulsion System (IPS) for Dawn will be used for the heliocentric transfer from the Earth to Vesta, orbit capture at Vesta, transfer to a low Vesta orbit, departure and escape from Vesta, the heliocentric transfer from Vesta to Ceres, orbit capture at Ceres, and transfer to a low Ceres orbit.


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    Titel :

    The ion propulsion system for Dawn


    Beteiligte:
    Brophy, J. R. (Autor:in) / Marcucci, M. G. (Autor:in) / Ganapathi, G. B. (Autor:in) / Garner, C. E. (Autor:in) / Henry, M. D. (Autor:in) / Nakazono, B. (Autor:in) / Noon, D. (Autor:in)

    Kongress:

    2003 Joint Propulsion Conference


    Erscheinungsdatum :

    2003-07-20


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    The Ion Propulsion System for Dawn

    Brophy, John / Garner, Charles / Nakazono, Barry et al. | AIAA | 2003


    Status of the Dawn Ion Propulsion System

    Brophy, John / Marcucci, Michael / Gates, Jason et al. | AIAA | 2004


    Implementation of the dawn ion propulsion system

    Brophy, John / Marcucci, Michael G. / Ganapath, Gani B. et al. | NTRS | 2005



    Dawn Ion Propulsion System - Initial Checkout After Launch

    Brophy, John / Garner, Charles / Mikes, Steven | AIAA | 2008