Total mission fuel and installed propulsion system weight are sensitive to choice of engine size and cycle, fuel type, and reserve fuel definition; effects of these variables on vehicle mission elements and on operational characteristics such as community noise, sonic boom, and flexibility as required by air traffic are studied; parameters evaluated are candidate engine cycles, effect of engine airflow in pounds per second, effect of propulsion system weight, and fuel consumption characteristics; sizing and cycle comparisons; study shows that engines will be sized by community noise or sonic boom considerations; other findings.


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    Titel :

    Propulsion systems sizing criteria for supersonic transport


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Drell, H. (Autor:in) / Bragdon, E.L. (Autor:in)

    Kongress:

    SAE Meeting ; 1965



    Erscheinungsdatum :

    1965


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Propulsion Systems Sizing Criteria for the Supersonic Transport

    Bragdon, E. L. / Drell, Harry | SAE Technical Papers | 1965


    Advanced Supersonic Transport Propulsion Systems

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


    Supersonic transport propulsion requirements

    Nichols, M.R. | Engineering Index Backfile | 1961