The Space Shuttle Orbiter air data system has been subjected to wind tunnel testing including three subsonic tests and one reference probe calibration test in order to obtain preflight calibration. Calibration curves for angle of attack, static pressure, and total pressure are given in the 0.35-0.55 Mach number range which represents flight conditions. The major difficulties encountered concerned the reference pressure of the facility, model-probe scale discrepancies, tunnel changes and blockage effects. Actual flight data calibrations from the approach and landing test program were used to modify the wind tunnel calibrations.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Wind tunnel and flight calibration of the Shuttle Orbiter air data system


    Contributors:

    Conference:

    Aerodynamic Testing Conference ; 1978 ; San Diego, CA


    Publication date :

    1978-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English






    Wind Tunnel Measurements of Shuttle Orbiter Global Heating with Comparisons to Flight

    S. A. Berry / N. R. Merski / R. C. Blanchard | NTIS | 2002


    Wind Tunnel Measurements of Shuttle Orbiter Global Heating With Comparison to Flight

    Berry, Scott / Merski, Norman / Blanchard, Robert | AIAA | 2002


    Wind Tunnel Measurements of Shuttle Orbiter Global Heating with Comparisons to Flight

    Berry, Scott A. / Merski, N. Ronald / Blanchard, Robert C. | NTRS | 2002