The development of two experimental burners was completed as part of a project to evaluate the suitability of the use of converted reciprocating engine turbochargers as expendable jet engines for remotely piloted vehicles. As a result of analytic studies, Burner 'A' was constructed as a reverse flow burner and was designed to accept a mass flow up to 0.75 lbm/sec. Burner 'B' was also reverse and designed for a mass flow up to 1.5 lbm/sec. Both burners operated successfully on their respective turbochargers.


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    Title :

    Combustor design for low cost expendable turbojets


    Additional title:

    Auslegung der Brennduesen fuer unaufwendige Strahltriebwerke


    Contributors:

    Published in:

    Publication date :

    1976


    Size :

    56 Seiten


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




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    Finch, V.C. | Engineering Index Backfile | 1948


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    Fuels for turbojets and ramjets.

    Hibbard, R. R. / Olson, W. T. | NTRS | 1964