An investigation has been made at a Mach number of 2.01 to determine the effects of a flared rudder on the aerodynamic characteristics of an ogee-wing space-shuttle orbiter configuration. Also investigated were the effects of an upper-aft fuselage fairing for the orbital maneuvering system, elevon deflections, and rudder deflection on the aerodynamic characteristics of the configuration.


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    Titel :

    Aerodynamic Characteristics of an Ogee-Wing Space Shuttle Orbiter Concept at a Mach Number of 2.01


    Beteiligte:
    L. E. Putnam (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    31 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch