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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    Titel :

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


    Beteiligte:
    A. D. Sappey (Autor:in) / L. Sutherland (Autor:in) / D. Owenby (Autor:in) / P. VanHoudt (Autor:in) / J. Hannam (Autor:in)

    Erscheinungsdatum :

    2009


    Format / Umfang :

    51 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Masterson, Bernard / Sappey, Andrew / Owenby, David et al. | AIAA | 2009


    Flight-Ready TDLAS Combustion Sensor for Hypersonics

    Masterson, P. / Sappey, A. / Owenby, D. et al. | British Library Conference Proceedings | 2009


    Development of a Flight-Worthy TDLAS-Based Oxygen Sensor for HIFiRE-1

    Sappey, Andrew / McCormick, P / Masterson, Pat et al. | AIAA | 2009



    Numerical Investigation of Hypersonic Phenomena Encountered in HIFiRE Flight 1

    Yentsch, R. / Gaitonde, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012