Paper shows how analog and digital computers are used to finalize thermal design calculations, with emphasis on effect of propellant-liner incremental thickness lumped with motor case, and how it is selected; effect of neglecting motor case heat storage on final temperature distribution is indicated for ground and flight analyses; results of comparative checks between analog, digital, and exact solutions are discussed; present exact solutions are limited and can only be considered as rough approximations during long ground standby times.


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    Titel :

    Solid propellant rocket motor thermal analysis


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Heatherly, E.R. (Autor:in) / Gonzalez, J.K. (Autor:in)

    Kongress:

    SAE Meeting ; 1962



    Erscheinungsdatum :

    1962


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Solid Propellant Rocket Motor Thermal Analysis

    Heatherly, E. R. / Gonzalez, J. I. | SAE Technical Papers | 1962


    SOLID PROPELLANT ROCKET MOTOR

    W. L. Dowler / J. I. Shafer / J. W. Behm et al. | NTIS | 1971


    Solid propellant rocket motor

    Dowler, W. L. / Shafer, J. I. / Behm, J. W. et al. | NTRS | 1973


    Solid Propellant Rocket Motor

    W. L. Dowler / J. I. Shafer / J. W. Behm et al. | NTIS | 1973