Problem of determining rocket trajectories of minimum propellant expenditure in absence of aerodynamic forces, is expressed as problem of Mayer type in calculus of variations; it is shown that method suggested by Cicala leads to some criteria obtained previously for case of rocket moving in vacuo, provided motor thrust is unlimited in magnitude; general criteria applicable when motor thrust cannot exceed certain magnitude was also found.


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    Titel :

    Necessary conditions for optimal rocket trajectories


    Weitere Titelangaben:

    Quarterly J Mechanics Applied Mathematics


    Beteiligte:
    Lawden, D.F. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    12 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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