Sets of equations presented may be used for calculating complete trajectories of satellites from outer space to ground under influence of air drag and gravity, including oblateness effects, and to apply these to several examples of entry trajectories starting from circular orbit.


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    Title :

    Three-dimensional orbits of earth satellites, including effects of earth oblateness and atmospheric rotation


    Additional title:

    NASA -- Memo


    Contributors:


    Publication date :

    1958


    Size :

    85 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :