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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    Titel :

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


    Beteiligte:
    A. M. inger (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    39 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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