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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    Titel :

    Approximate solutions to optimum climbing trajectory for rocket-powered aircraft


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Miele, A. (Autor:in) / Cappellari, Jr., J.O. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    56 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Optimum climbing technique for rocket-powered aircraft

    Miele, A. | Engineering Index Backfile | 1955



    Climbing performance analysis of rocket-based combined cycle engine powered aircraft

    Jia, Yicong / Ye, Wei / Cui, Peng et al. | Elsevier | 2019