A jet aircraft includes an aircraft integrated, fluid vectoring, exhaust nozzle system. Implementation of this disclosure may eliminate or reduce the size of the aircraft vertical stabilizer and rudder assembly, thereby potentially improving aircraft survivability and increasing aircraft thrust-to-weight ratio.


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    Title :

    FLUID-VECTORING SYSTEM


    Additional title:

    FLUIDVEKTORISIERUNGSSYSTEM
    SYSTÈME DE VECTORISATION DE FLUIDE


    Contributors:
    BAKER VON D (author)

    Publication date :

    2020-09-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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