NASA's proposed mission to send a single electric propulsion spacecraft to orbit Callisto, Ganymeds, and Europa within a decade would require a very complex trajectory. Strong multi-body effects combined with low-thrust control of capture and escape will make the trajectory challenging. This paper describes an optimal trajectory that begins in low Earth orbit and ends in low Io orbit.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    An investigation of a Jupiter Galilean Moon Orbiter trajectory


    Contributors:

    Conference:

    2003 AAS/AIAA Astrodynamics Specialist Conference ; 2003 ; Big Sky, MT, United States


    Publication date :

    2003-08-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    An Investigation of a Jupiter Galilean Moon Orbiter Trajectory (AAS 03-544)

    Whiffen, G. J. / American Astronautical Society | British Library Conference Proceedings | 2004




    Galilean satellite remote sensing by the Galileo Jupiter Orbiter

    Yeates, C. M. / Klaasen, K. P. / Clarke, T. C. | NTRS | 1983