Methods for calculating ballistic behavior of hybrid propellant combinations; effects of scaling, pressure level, and internal geometric configuration are examined, using machine analysis that is based upon heat-transfer-limited theory; crucial aspect of efficient hybrid grain design is proper matching of surface area progressivity to regression rate-mass flux dependence; interaction between convective and radiative modes of heat transfer and general aspects of throttling are also considered; regimes of operation where heat-transfer-limited theory begins to break down are delineated.


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    Title :

    Internal ballistic considerations in hybrid rocket design


    Additional title:

    J Spacecraft Rockets


    Contributors:

    Published in:

    Publication date :

    1967


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





    Internal ballistic considerations in hybrid rocket design

    MUZZY, R. / WOOLDRIDGE, C. | AIAA | 1966


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