This report was prepared to document a study of optimum weight ratios of multi-stage rockets. The study includes the effects of gravity and of stage inert weights expressed as a constant plus a term proportional to stage propellant weight. This report includes the case of no gravity field and the case of vertical flight in a constant gravity field. A subsequent report will present the case of general ballistic flight in a constant gravity field. (Author)


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    Titel :

    Analysis of Optimum Staging Ratios for Rockets with Fixed and Propellant-Dependent Structural Factors


    Beteiligte:
    F. R. Sedlund (Autor:in)

    Erscheinungsdatum :

    1960


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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