This paper presents the results of recent Douglas Aircraft Company integration studies for an advanced supersonic transport. The studies include technology improvements such as superplastic formed and diffusion-bonded titanium sandwich primary structure, composite secondary structure, bicone engine inlet, improved mechanical suppressors based on flight test data, improved aerodynamic efficiency based on wind tunnel test data, and updated performance for both variable-cycle and low-bypass-ratio engines. Technology development requirements for an economically viable and environmentally acceptable advanced supersonic transport are defined through these studies. A new Douglas Aircraft Company baseline supersonic transport designed to carry 350 passengers is defined for cost comparisons.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Advanced supersonic transport propulsion and configuration technology improvements


    Contributors:
    Rowe, W. T. (author) / Welge, H. R. (author) / Johnson, E. S. (author) / Rochte, L. S. (author)

    Conference:

    Joint Propulsion Conference ; 1981 ; Colorado Springs, CO, US


    Publication date :

    1981-07-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Advanced supersonic transport propulsion and configuration technology improvements

    ROWE, W. / WELGE, H. / JOHNSON, E. et al. | AIAA | 1981


    Advanced Supersonic Transport Propulsion Systems

    Smith, Martin G. / Howlett, Robert A. | SAE Technical Papers | 1977



    Benefits of Advanced Propulsion Technology for the Advanced Supersonic Transport

    Sabatella, Joseph A. / Hines, Richard W. | SAE Technical Papers | 1973