Trajectory and mission requirement data are presented for Earth Mars opposition and conjunction class roundtrip flyby and stopover mission opportunities available between 1997 and 2045. The opposition class flyby mission uses direct transfer trajectories to and on return from Mars. The opposition class stopover mission employs the gravitational field of Venus to accelerate the space vehicle on either the outbound or inbound leg in order to reduce the propulsion requirement associated with the opposition class mission. The conjunction class mission minimizes propulsion requirements by optimizing the stopover time at Mars.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Mars Mission Concepts and Opportunities


    Contributors:

    Conference:

    Manned Mars Missions Workshop ; 1985 ; Huntsville, AL, US



    Publication date :

    1986-05-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





    Crewed Mars Mission Concepts

    Mike Meyer | NTRS | 2022



    Mars Pathfinder Mission Operations Concepts

    Tai, W. / Nakata, A. / Dias, W. et al. | NTRS | 1994


    Manned Mars Mission program concepts

    Hamilton, E. C. / Johnson, P. / Pearson, J. et al. | NTRS | 1988