Details of X-15 arrangement and flight control system; aerodynamic surfaces for control consist of upper and lower verticals; trailing edges of upper and lower fixed portions deflect as speed brakes; reaction control rockets are located in nose for pitch and yaw and at wing tips for roll; propellant supply system; evaluation and test data obtained on flight control system; current status of flight test program; expected performance capabilities. (See also SAE -- Paper n S-247 for meeting v 68 n 8 Mar 24 1960 9 p)


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    Titel :

    X-15 -- Reaction control aircraft


    Weitere Titelangaben:

    SAE -- J


    Beteiligte:
    Merrick, G.B. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    X-15 -- Reaction control aircraft

    Merrick, G.B. | Engineering Index Backfile | 1960


    Reaction Control Systems for V/STOL Aircraft

    Thames, W. K. | SAE Technical Papers | 1965


    THE X-15-A REACTION CONTROL AIRCRAFT

    MERRICK, GEORGE B. | SAE Technical Papers | 1960


    Aircraft reaction link

    ITOH KOJI / OGAWA TOSHIAKI / NAGASHIMA MAKOTO | Europäisches Patentamt | 2017

    Freier Zugriff

    Reaction control system augmentation for V/STOL aircraft

    Streiff, H. G. / Donham, R. E. | NTRS | 1979