Technique of trajectory and stage propellant loading optimization for powered phase of multistage rocket carriers through atmosphere is presented; procedure is particularly suitable for large scale engineering analyses of vehicle trajectories and performance by means of digital computers; theoretical requirements and equations of motion are considered; basic computer program logic is described; technique is applied to hypothetical 2- and 3-stage vehicle in Saturn V class.


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    Titel :

    Technique for optimization of ascent trajectories and propellant loadings of multistage space vehicles


    Weitere Titelangaben:

    Raumfahrtforschung


    Beteiligte:
    Thomae, H.F. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1964


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :