Sonic boom pressure signatures were measured in supersonic and hypersonic wind tunnels for models of the space shuttle launch vehicle at 0 deg angle of attack with and without solid body simulations of the exhaust plumes. Data were measured at 30 deg increments in roll angle from 90 deg to 180 deg at Mach numbers from 3.02 to 5.56. (Author)


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    Title :

    Sonic Boom Pressure Signatures for the Space Shuttle Launch Vehicle


    Contributors:

    Publication date :

    1975


    Size :

    73 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English