Experimental investigation of the problems associated with restarting hybrid rocket motors (i.e., motors wherein a liquid or gaseous oxidizer is injected into the port of a solid fuel grain with subsequent mixing and combustion of the oxidizer and fuel) following a brief period of extinguishment. The results include the finding that the ignition delay on restart is decreased because less energy is absorbed by the fuel before the surface reaches the ignition point.


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    Titel :

    Restart transients of hybrid rocket engines.


    Beteiligte:
    Saraniero, M. A. (Autor:in) / Caveny, L. H. (Autor:in) / Summerfield, M. (Autor:in)


    Erscheinungsdatum :

    01.03.1973


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Restart transients of hybrid rocket engines.

    SARANIERO, M. A. / CAVENY, L. H. / SUMMERFIELD, M. | AIAA | 1973


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