An engineering examination is made of a subsonic analog of the F-111A to determine what savings can be made in terms of weight and cost. It is concluded that so long as both planes have the same mission, both planes will have nearly the same gross takeoff weight. Savings in cost appear to be substantial, however, and a detailed cost analysis is being prepared for sepetate distribution. (Author)


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    Titel :

    A Subsonic Analog of the F-111A Airplane


    Beteiligte:
    R. D. Linnell (Autor:in)

    Erscheinungsdatum :

    1964


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch