Presented in this report are the results of an investigation to evaluate aerodynamically the use of very low aspect-ratio fins, capped fins and shrouded fins to provide flight stability for the hypervelocity air-to-ground rocket (HAGR) configuration. Static-stability data were obtained for the HAGR configurations at Mach numbers ranging from 0.9 to 7.71.


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    Title :

    Preliminary Wind Tunnel Investigation of the HAGR Configurations at Transonic, Supersonic and Hypersonic Mach Numbers


    Contributors:

    Publication date :

    1966


    Size :

    58 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English