X-15 performance envelope is shown; paper considers operational phase of X-15 and major thermal structural problems encountered, such as landing gear overloading, panel flutter, side-fairing buckling, wing leading-edge skin buckling, windshield heat damage, and internal heat damage; role played by various simulators used in design and operational phases; 3 major accidents which occurred show significance that single malfunction can have in imposing marginal conditions on another system.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    X-15 flight-test experience


    Weitere Titelangaben:

    Astronautics Aerospace Eng


    Beteiligte:
    Row, P.V. (Autor:in) / Fischel, J. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Lift fan flight test experience

    CLARK, D. / SMITH, E. | AIAA | 1965


    YJ101/YF-17 Flight Test Experience

    RAPP, G. C. / LAIL, G. G. / MONTGOMERY, J. F. | SAE Technical Papers | 1976


    Experience with flight test trajectory guidance

    Swann, M. R. / Duke, E. L. / Enevoldson, E. K. et al. | NTRS | 1981


    Experience with flight test trajectory guidance

    Duke, E. L. / Swann, M. R. / Enevoldson, E. K. et al. | NTRS | 1983


    Experience with flight test trajectory guidance

    DUKE, E. L. / SWANN, M. R. / ENEVOLDSON, E. K. et al. | AIAA | 1983