Effects of torques due to aerodynamic drag and gravity gradient are computed for satellites orbiting at altitudes of between 80 and 375 mi; equilibrium position is determined as function of altitude for both dumbbell and cylindrical-shaped object; equilibrium position of cylindrical object in three dimensions is considered as function of altitude; equations.


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    Titel :

    Effect of aerodynamic forces on satellite attitude


    Weitere Titelangaben:

    J Astronautical Sciences


    Beteiligte:
    DeBra, D.B. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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