A procedure for automatically designing a liquid propellant rocket engine combustion chamber in an optimal fashion is outlined. The procedure is contained in a digital computer code, AUTOCOM. The code is applied to an existing engine, and design modifications are generated which provide a substantial potential payload improvement over the existing design. Computer time requirements for this payload improvement were small, approximately four minutes in the CDC 6600 computer.


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    Titel :

    Optimizing a liquid propellant rocket engine with an automated combustor design code (AUTOCOM)


    Beteiligte:
    Hague, D. S. (Autor:in) / Reichel, R. H. (Autor:in) / Jones, R. T. (Autor:in) / Glatt, C. R. (Autor:in)

    Erscheinungsdatum :

    01.12.1972


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :