The flight testing techniques and analyses used to verify the stability and control characteristics of the Space Shuttle Orbiter are examined. The pods of the reaction control system jets, the elevon panels, bodyflap, rudder, and automatic flight control system, which provide pitch, yaw, and roll control and thermal protection for the Orbiter, are described. The control maneuvers of the Shuttle are analyzed using the modified maximum likelihood estimator. Approach and landing and flight test data are applied to the study of the instrumentation, and to the evaluation of the stability and control characteristics of the Orbiter.


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    Titel :

    Aerodynamic flight testing of the Space Shuttle Orbiter


    Beteiligte:
    Barton, R. L. (Autor:in) / Culp, M. A. (Autor:in)

    Erscheinungsdatum :

    01.01.1985


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Aerodynamic Flight Testing of the Space Shuttle Orbiter

    Culp, Micheal A. / Barton, Richard L. | SAE Technical Papers | 1985


    Space Shuttle Orbiter and Aerodynamic Testing

    Paul M.Siemers Terry J. Larson | AIAA | 1979


    The Space Shuttle Orbiter and aerodynamic testing

    Siemers, P. M., III / Larson, T. J. | NTRS | 1978


    The Space Shuttle Orbiter and aerodynamic testing

    SIEMERS, III, P. / LARSON, T. | AIAA | 1978


    Space Shuttle orbiter aerodynamic development

    SURBER, T. / OLSEN, D. | AIAA | 1974