Two computer programs calculate interaction effects of high speed spacecraft on the environment at altitudes from 90 km to 150 km. EXT program determines fluid field in bodies of arbitrary geometries in transient flow regime. INT program uses EXT output and measures flow conditions inside spacecraft body.


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    Title :

    A low-altitude satellite interaction study


    Contributors:

    Publication date :

    1971-12-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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