The reported investigation has the objective to show how a loosely constrained set of mission design parameters can be analyzed to design trajectories that can satisfy both science and mission requirements. A description is presented of methods for handling several loosely constrained mission design parameters. An example trajectory design is generated. It is found that tradeoffs exist between science payload, maximum heliographic latitude, and the particular trajectory design strategy selected. An analysis shows that even with the help of contour plots, judicious specifications of constraints for the mission design parameter values will be necessary if the mission design process is to be manageable.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Trajectory design aspects of a proposed NASA/ESA Out-of-Ecliptic mission


    Contributors:

    Conference:

    Astrodynamics Specialist Conference


    Publication date :

    1977-09-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English