A progress report is given on a research project to use the microwave Doppler velocimeter technique to measure the combustion response to an oscillating thermal radiation source (CO2 laser). The test technique and supporting analyses are described, and the results are presented for an initial test series on the nonmetallized, composite propellant, Naval Weapons Center formulation A-13. It is concluded that in-depth transmission of radiant heat flux is not a factor at the CO2 laser wave length.


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    Titel :

    Solid propellant combustion response to oscillatory radiant heat flux


    Beteiligte:
    Strand, L. D. (Autor:in) / Weil, M. T. (Autor:in) / Cohen, N. S. (Autor:in)

    Erscheinungsdatum :

    01.07.1989


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Solid propellant combustion response to oscillatory radiant heat flux

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


    Propellant combustion response to oscillatory radiant heat flux

    Strand, L. D. / Schwartz, K. / Burns, S. P. | NTRS | 1987


    Measurement of propellant combustion response to sinusoidal radiant heat flux

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


    Measuring Response Of Propellant To Oscillatory Heat Flux

    Strand, Leon D. / Schwartz, Ken / Burns, Shawn P. | NTRS | 1990