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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    Titel :

    Sonic Boom Pressure Signatures for the Space Shuttle Launch Vehicle


    Beteiligte:
    J. P. Mendoza (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    73 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch