Apparatus for research in combustion of solid propellants measures oscillatory response of rate of burning to oscillating thermal radiation from modulated CO2 laser. Determines response to rate of burning to equivalent oscillation in pressure. Rod of propellant mounted in burner assembly including waveguide at one end and infrared window at other end. Microwave Doppler velocimeter measures motion of combustion front. Microwave, laser-current, and heat-flux signals processed into and recorded in forms useful in determining desired response of propellent.


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    Titel :

    Measuring Response Of Propellant To Oscillatory Heat Flux


    Beteiligte:
    Strand, Leon D. (Autor:in) / Schwartz, Ken (Autor:in) / Burns, Shawn P. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.10.1990



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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    STRAND, L. / WEIL, M. / COHEN, N. | AIAA | 1989


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    FINLINSON, J. / HANSON-PARR, D. / SON, S. et al. | AIAA | 1991


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