Rocket engine exhaust gas temperature and spectral emission are important in design and development of rocket engines; technique of monochromatic radiation pyrometry and instrumentation for applying technique were developed; results of 9 rocket engine firings are presented.


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    Title :

    Determination of rocket exhaust gas temperatures and emissivities by infrared spectral methods


    Additional title:

    SAE -- Paper


    Contributors:
    Penzias, G.J. (author) / Dolin, S.A. (author) / Tourin, R.H. (author)

    Conference:

    SAE Meeting ; 1962 Exhaust gases



    Publication date :

    1962


    Size :

    4 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :