It is shown that fairly accurate optimum thrusts can be calculated by including the effect of rocket-engine weight while neglecting aerodynamic drag. The results for vertical take-off with constant thrust in a constant gravity field are presented for optimization to obtain maximum burnout velocity or maximum burnout energy. (Author)


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    Titel :

    Optimum Thrusts for Rockets in Vertical Flight in Vacuum


    Beteiligte:
    R. D. Linnell (Autor:in)

    Erscheinungsdatum :

    1960


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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