This paper reviews recent progress in the key hypersonic technologies, which has been good despite a relatively low priority. Successful hypersonic research engine tests have been made. Active cooling system analyses have shown potential for weight savings, alleviation of structural design problems, and long airframe life. Maturing computerized flow field theories permit optimizing engine-airframe performance. Adequate progress in the future requires an expanded technology program emphasizing hydrogen usage. A hydrogen fueled hypersonic research airplane is essential, providing critical flight data and operational experience.


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    Title :

    Key technology for airbreathing hypersonic aircraft.


    Contributors:

    Conference:

    Annual Meeting and Technical Display ; 1973 ; Washington, DC


    Publication date :

    1973-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Key technology for airbreathing hypersonic aircraft

    NAGEL, A. / BECKER, J. | AIAA | 1973



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    J. L. Hunt / P. L. Lawing / D. C. Marcum | NTIS | 1978



    Hypersonic airbreathing propulsion

    Avery, W.H. / Dugger, G.L. | Engineering Index Backfile | 1964