Relatively simple and straightforward method of determining this trade off and some typical trade off values are given; method is general with respect to vehicle performance or design criteria and is illustrated for case where multistage vehicle's inert parts weights and propellant volumes are fixed and given vehicle burnout velocity is to be maintained.


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    Titel :

    Trade-off between propellant specific impulse and density


    Weitere Titelangaben:

    Aerospace Eng


    Beteiligte:
    Gordon, L.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1961


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    HIGH IMPULSE DENSITY COMPOSITE PROPELLANT SYSTEMS

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    Specific impulse prediction of solid propellant motors

    LANDSBAUM, E. / SALINAS, M. / LEARY, J. | AIAA | 1979


    Specific Impulse Prediction of Solid-Propellant Motors

    E.M. Landsbaum / M.P. Salinas / J.P. Leary | AIAA | 1980