This 3-volume report discusses the evaluation of aerothermal flight measurements made on the orbital flight test Space Shuttle External Tanks (ETs). Six ETs were instrumented to measure various quantities during flight; including heat transfer, pressure, and structural temperature. The flight data was reduced and analyzed against math models established from an extensive wind tunnel data base and empirical heat-transfer relationships. This analysis has supported the validity of the current aeroheating methodology and existing data base; and, has also identified some problem areas which require methodology modifications. Volume 1 is the Executive Summary. Volume 2 contains Appendix A (Aerothermal Comparisons), and Appendix B (Flight-Derived h sub 1/h sub u vs. M sub inf. Plots). This is Volume 3, containing Appendix C (Comparison of Interference Factors between OFT Flight, Prediction and 1H-97A Data), Appendix D (Freestream Stanton Number and Reynolds Number Correlation for Flight and Tunnel Data), and Appendix E (Flight-Derived h sub i/h sub u Tables).


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    Title :

    Orbital flight test shuttle external tank aerothermal flight evaluation, volume 3


    Contributors:

    Publication date :

    1986-06-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Orbital flight test shuttle external tank aerothermal flight evaluation, volume 2

    Praharaj, Sarat C. / Engel, Carl D. / Warmbrod, John D. | NTRS | 1986


    Orbital Flight Test Shuttle External Tank Aerothermal Flight Evaluation, Volume 1

    S. C. Praharaj / C. D. Engel / J. D. Warmbrod | NTIS | 1986


    Orbital flight test shuttle external tank aerothermal flight evaluation, volume 1

    Praharaj, Sarat C. / Engel, Carl D. / Warmbrod, John D. | NTRS | 1986