An assessment is done of current and potential ground facilities, and analysis and flight test techniques for establishing a hypersonic propulsion/airframe integration technology base. A mach 6 cruise prototype aircraft incorporating integrated Scramjet engines was considered the baseline configuration, and the assessment focused on the aerodynamic and configuration aspects of the integration technology. The study describes the key technology milestones that must be met to permit a decision on development of a prototype vehicle, and defines risk levels for these milestones. Capabilities and limitations of analysis techniques, current and potential ground test facilities, and flight test techniques are described in terms of the milestones and risk levels.


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    Titel :

    Study of Hypersonic Propulsion/Airframe Integration Technology


    Beteiligte:
    W. R. Hartill (Autor:in) / T. P. Goebel (Autor:in) / V. V. Vancamp (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    97 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Study of hypersonic propulsion/airframe integration technology

    Hartill, W. R. / Goebel, T. P. / Vancamp, V. V. | NTRS | 1978




    A HYPERSONIC PROPULSION AIRFRAME INTEGRATION OVERVIEW

    Lewis, M. J. / American Institute of Aeronautics and Astronautics / Society of Automotive Engineers et al. | British Library Conference Proceedings | 2003