Results of X-15 Program pertaining to terminal phase of flight and how these can be useful in developing horizontal landing techniques for future gliding re-entry vehicles; X-15 is stubby-winged rocket powered aircraft which is air launched from B-52mother ship; development of techniques and some flight test results; effects of wing loading, lift-drag ratio, visibility, handling qualities, speed brakes, and trim changes are analyzed as they pertain to low lift/ drag landings of X-15 and other configurations; use of in-flight landing simulator to provide pilot training and maintain pilot proficiency is emphasized.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Horizontal landing techniques for hypersonic vehicles


    Weitere Titelangaben:

    AGARD -- Report


    Beteiligte:
    Hoey, R.G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Aeroservoelastic stabilization techniques for hypersonic flight vehicles

    Chan, Samuel Y. / Cheng, Peter Y. / Pitt, Dale M. et al. | NTRS | 1991


    Aeroservoelastic stabilization techniques for hypersonic flight vehicles

    Cheng, Peter Y. / Chan, Samuel Y. / Myers, Thomas T. et al. | NTRS | 1991


    Aeroservoelastic stabilization techniques for hypersonic flight vehicles

    CHENG, PETER / CHAN, SAMUEL / MYERS, THOMAS et al. | AIAA | 1991


    Thrust vectoring for single-stage-to-orbit, horizontal takeoff, horizontal landing, space vehicles

    Cunningham, M. J. / Freeman, D. C., Jr. / Wilhite, A. W. et al. | NTRS | 1986


    Thrust vectoring for single-stage-to-orbit, horizontal takeoff, horizontal landing, space vehicles

    CUNNINGHAM, M. / FREEMAN, JR., D. / WILHITE, A. et al. | AIAA | 1986