The technological status of a boron-slurry and the low-volume ramjet engines was reviewed. Engine performance maps including parametric variations of the critical assumptions were developed. Numerous preliminary designs of the ARM-II missile system utilizing each propulsion system were made. The range performance for a low-altitude, high-speed trajectory was calculated for each design and its parametric variations. The results show the boron-slurry engine offers a substantial range performance advantage over the low-volume ramjet engine for both the weight and volume limited cases.


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    Title :

    Comparison of Advanced Ramjet Engines


    Contributors:
    R. H. Traver (author) / H. O. Porter (author)

    Publication date :

    1965


    Size :

    40 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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