A launch phase random normal wind model is presented for delta wing, two-stage, space shuttle control system studies. Equations, data, and simulations for conventional launch studies are given as well as pitch and lateral equations and data for covariance analyses of the launch phase of MSFC vehicle B. Lateral equations and data for North American 130G and 134D are also included along with a high-altitude abort simulation.


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    Title :

    Development of control systems for space shuttle vehicles. Volume 2: Appendixes


    Contributors:
    Stone, C. R. (author) / Chase, T. W. (author) / Kiziloz, B. M. (author) / Ward, M. D. (author)

    Publication date :

    1971-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :