Problem of determination of optimum climbing technique from one combination of altitude and velocity to another is considered; climbing program is analyzed with regard to minimum time trajectories; effect of important design parameters, such as wing or thrust loading on solutions is investigated.


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    Title :

    Approximate solutions to optimum climbing trajectory for rocket-powered aircraft


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1959


    Size :

    56 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



    Optimum climbing technique for rocket-powered aircraft

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