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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Comparison of Advanced Ramjet Engines


    Beteiligte:
    R. H. Traver (Autor:in) / H. O. Porter (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    40 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Control system requirements for advanced ramjet engines

    HARNER, K. / PATRICK, J. | AIAA | 1978


    Ramjet Engines Performance

    Ingenito, Antonella | Springer Verlag | 2021



    A fluidic fuel control for advanced ramjet engines

    CHAPIN, D. / SCHEER, L. / WALDON, B. | AIAA | 1980


    Fundamentals of Ramjet Engines

    Ingenito, Antonella | Springer Verlag | 2021