Research on a new, hydrogen burning, airbreathing engine concept which offers good potential for efficient hypersonic cruise vehicles is considered. Features of the engine which lead to good performance include; extensive engine-airframe integration, fixed geometry, low cooling, and the control of heat release in the supersonic combustor by mixed-modes of fuel injection from the combustor entrance. The engine concept is described along with results from inlet tests, direct-connect combustor tests, and tests of two subscale boiler-plate research engines presently underway at conditions which simulate flight at Mach 4 and 7.


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    Titel :

    Airframe-integrated propulsion system for hypersonic cruise vehicles


    Beteiligte:
    Jones, R. A. (Autor:in) / Huber, P. W. (Autor:in)

    Kongress:

    Congr. of the Intern. Council of the Aeron. Sci. ; 1978 ; Lisbon



    Erscheinungsdatum :

    01.01.1978


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :