Advanced air-breathing engine development requires new combustion diagnostics. The new sensors must not intrude into the engine and the sensing components must endure the thermal and vibrational environment near a scramjet combustor. The sensor should also be suitable as a diagnostic in realistic scramjet test situations, including in flight in sounding-rocket test vehicles. The development of a laser sensor meeting these requirements for the HIFiRE 2 hypersonic research program is described in this report.


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    Title :

    Flight-Ready TDLAS Combustion Sensor for the HIFiRE 2 Hypersonic Research Program


    Contributors:
    A. D. Sappey (author) / L. Sutherland (author) / D. Owenby (author) / P. VanHoudt (author) / J. Hannam (author)

    Publication date :

    2009


    Size :

    51 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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