Computer program for optimum flight path defined by flight test investigation of performance characteristics /excess thrust, fuel flow, and climb potential/ of F-104G aircraft


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    Title :

    Flight determined acceleration and climb performance of an F-104G airplane for use in an optimum flight path computer program


    Contributors:

    Publication date :

    1971-06-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :