Structural temperatures and thermal protection system surface temperatures were measured on the space shuttle during the flight of STS 5. The measured data are compared with values calculated at wing stations 134, 240, and 328 and at fuselage station 877. The theoretical temperatures were calculated using the structural performance and resizing finite element thermal analysis program. The comparisons show that the calculated temperatures are, generally, in good agreement with the measured data.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Comparison of flight-measured and calculated temperatures on the space shuttle orbiter


    Beteiligte:
    Gong, Leslie (Autor:in) / Ko, William L. (Autor:in) / Quinn, Robert D. (Autor:in) / Richards, W. Lance (Autor:in)

    Erscheinungsdatum :

    01.11.1987


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Space shuttle orbiter test flight series

    Garrett, D. / Gordon, R. / Jackson, R. B. | NTRS | 1977


    Flight problem evaluation for Space Shuttle Orbiter

    Mechelay, Joseph E. / Ward, Robert J. | NTRS | 1987


    Aerodynamic flight testing of the Space Shuttle Orbiter

    Barton, R. L. / Culp, M. A. | NTRS | 1985


    Space Shuttle Orbiter Auxiliary Power Unit Flight Performance

    Weary, D. / Baughman, J. / Wicklund, L. et al. | SAE Technical Papers | 1982