Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Free-flight Investigation at Mach Numbers Between 0.5 and 1.7 of the Zero-lift Rolling Effectiveness and Drag of Various Surface, Spoiler, and Jet Controls on an 80 Degree Delta-wing Missile


    Contributors:

    Publication date :

    1956-11-29


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English