For interplanetary missions, highly efficient electric propulsion systems can be used to increase the mass delivered to the destination and/or reduce the trip time over typical chemical propulsion systems.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Preliminary Design of Low-Thrust Interplanetary Missions


    Contributors:
    Flanagan, S. (author) / Sims, J. (author)

    Publication date :

    1999-08-16


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





    Preliminary Design of Low-Thrust Interplanetary Missions

    Sims, Jon A. / Flanagan, Steve N. | NTRS | 1997


    Preliminary Design of Low-Thrust Interplanetary Missions

    J. A. Sims / S. N. Flanagan | NTIS | 1997


    Preliminary Design of Low-Thrust Interplanetary Missions (AAS 99-338)

    Sims, J. A. / Flanagan, S. N. / American Astronautical Society et al. | British Library Conference Proceedings | 2000


    Compensator Design for Low-Thrust Interplanetary Missions

    Fiehler, Douglas / Kluever, Craig | AIAA | 2002