A unique aircraft propulsive/lift power distribution system is described that promises a great deal of flexibility in the design of VTOL aircraft. Its use would permit a significant improvement in many aspects of present and future VTOL designs, including performance, safety, cost, operability, noise, applicability, and operational economy. (Author)


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    Titel :

    The Turbo-Electric VTOL Aircraft


    Beteiligte:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    79 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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