Investigation made in Langley supersonic pressure tunnel to measure effects of 2 sets of cruciform fins, of inline and indexed fin arrangements, flare, antennas, launch fittings, and control tunnels on aerodynamic characteristics of configuration for combined angles of attack and sideslip to about 8°.


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    Title :

    Aerodynamic characteristics in pitch and sideslip of 1/15-scale model of scout vehicle at mach number of 2.01


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    37 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English