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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Study of Hypersonic Propulsion/Airframe Integration Technology


    Contributors:

    Publication date :

    1978


    Size :

    97 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English