The primary purpose of this test was to determine discharge coefficients for both the center axial and radial 2:1 aspect ratio exhaust ports of the ASRM multi-port igniter. In addition, both ports were tested with chamfered leading edge to assess how much improvement in discharge coefficient could potentially be achieved.


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    Title :

    Posttest Report for the Advanced Solid Rocket Motor (ASRM) Igniter Discharge Port Flow Test


    Contributors:
    A. M. inger (author)

    Publication date :

    1993


    Size :

    39 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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