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    Title :

    Control of the space shuttle angle-of-attack during reentry


    Contributors:

    Publication date :

    2002


    Size :

    95 pages


    Remarks:

    Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2002.
    Includes bibliographical references (leaf 95).


    Type of media :

    Theses


    Type of material :

    Electronic Resource


    Language :

    English




    Reentry heating and flow fields for Space Shuttle Orbiter at high angle of attack

    ROCHELLE, W. / ROBERTS, B. / D'ATTORRE, L. et al. | AIAA | 1972



    Thermal Response of Space Shuttle Wing During Reentry Heating

    L. Gong / W. L. Ko / R. D. Quinn | NTIS | 1984


    Thermal response of Space Shuttle wing during reentry heating

    Gong, L. / Ko, W. L. / Quinn, R. D. | NTRS | 1984


    Thermal response of Space Shuttle wing during reentry heating

    GONG, L. / KO, W. / QUINN, R. | AIAA | 1984