Maximum payload is required for given vehicle; in variation problem, equations of movement of space vehicles occur as secondary condition; further conditions enter problem by technical limitations of propulsion; limiting cases of unbounded and constant thrust are considered; in both cases distinction must be made between flights with given time of takeoff in synodic year and those with open time of takeoff; time will be chosen so that payload becomes maximum.


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    Title :

    Optimization of interplanetary flights with vehicles of low thrust acceleration


    Additional title:

    Zur Optimalisierung interplanetarer Uebergangsbahnen mit kleiner Schubbeschleunigung


    Contributors:
    Roessger, E. (author) / Zehle, H. (author)


    Publication date :

    1963


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :