Flight data taken from three Shuttle Space Transportation System flights (STS-1, 2, and 3) during entry are analyzed to determine the shuttle performance and aerodynamic characteristics. Correlations of the performance coefficients and the stability and control derivatives with preflight predictions are presented over the hypersonic speed range from Mach 2 to 25. In addition, an evaluation of the effectiveness of the onboard Reaction Control System (RCS) is given and an effort is made to independently quantify the combined impingement and flow-field interaction effects on the spacecraft rolling moment. Comparisons of stability and control derivatives extracted for the same flight conditions, but using data from different onboard sensors are also made. Results obtained using the same flight data, but different computer software are also shown.


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    Titel :

    Shuttle entry performance and stability and control derivatives extraction from flight measurement data


    Beteiligte:
    Compton, H. R. (Autor:in) / Scallion, W. I. (Autor:in) / Schiess, J. R. (Autor:in) / Suit, W. T. (Autor:in)

    Kongress:

    Atmospheric Flight Mechanics Conference ; 1982 ; San Diego, CA


    Erscheinungsdatum :

    1982-08-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Space Shuttle stability and control derivatives estimated from the first entry

    ILIFF, K. W. / MAINE, R. E. / COOKE, D. R. | AIAA | 1983


    Space Shuttle stability and control derivatives estimated from the first entry

    Iliff, K. W. / Maine, R. E. / Cooke, D. R. | NTRS | 1983



    Selected stability and control derivatives from the first Space Shuttle entry

    Iliff, K. W. / Maine, R. E. / Cooke, D. R. | NTRS | 1981