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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    Titel :

    Optimization of interplanetary flights with vehicles of low thrust acceleration


    Weitere Titelangaben:

    Zur Optimalisierung interplanetarer Uebergangsbahnen mit kleiner Schubbeschleunigung


    Beteiligte:
    Roessger, E. (Autor:in) / Zehle, H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Deutsch


    Schlagwörter :



    Optimization methods of near-Earth and interplanetary flights with low thrust

    Salmin, V. V. / Starinova, O. L. / Volosuev, V. V. et al. | American Institute of Physics | 2017




    Interplanetary trajectories under low thrust radial acceleration

    Copeland, J. | Engineering Index Backfile | 1959