A parametric sensitivity analysis of the space shuttle ascent flight to the wind profile is presented. Engineering systems parameters are obtained by flight simulations using wind profile models and samples of detailed (Jimsphere) wind profile measurements. The wind models used are the synthetic vector wind model, with and without the design gust, and a model of the vector wind change with respect to time. From these comparison analyses an insight is gained on the contribution of winds to ascent subsystems flight parameters.


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    Title :

    Sensitivity analysis of the space shuttle to ascent wind profiles


    Contributors:

    Publication date :

    1982-03-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    Sensitivity analysis of the Space Shuttle to ascent wind profiles

    Smith, O. E. / Austin, L. D., Jr. | NTRS | 1981


    Space Shuttle response to ascent wind profiles

    Smith, O. E. / Austin, L. D., Jr. | NTRS | 1983


    Space Shuttle response to ascent wind profiles

    SMITH, O. E. / AUSTIN, L. D. | AIAA | 1983