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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    Title :

    The Turbo-Electric VTOL Aircraft


    Contributors:

    Publication date :

    1968


    Size :

    79 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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