A brief discussion is presented of the major problem areas involved in the development of a hypersonic ramjet engine. Keeping the structural temperature to an acceptably low level is the severest problem expected. A rapid survey is made of some of the relatively unconventional concepts that may find application in the hypersonic region. These include supersonic combustors, underwing burning, atmospheric-recombination, engine installation, nuclear power, variable geometry, and fuel-rich operation.


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    Titel :

    A Survey of Hypersonic-Ramjet Concepts


    Beteiligte:
    Weber, R. J. (Autor:in)

    Kongress:

    American Rocket society Semi-Annual Meeting ; 1959 ; San Diego, CA, United States


    Erscheinungsdatum :

    08.06.1959


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Detonation wave hypersonic ramjet

    Sargent, W.H. / Gross, R.A. | Engineering Index Backfile | 1960


    Ramjet Technology. Chapter 11. Hypersonic Ramjets

    G. L. Dugger / F. S. Billig | NTIS | 1970


    Hypersonic ramjet using normal detonation wave

    Arens, M. | Engineering Index Backfile | 1960


    Advanced ramjet concepts program

    Leingang, J. L. | NTRS | 1992