The results are presented of studies performed relating to the feasibility of deploying a subsatellite from the shuttle by means of a tether. The dynamics, the control laws, the aerodynamics, the heating, and some communication considerations of the tethered subsatellite system are considered. Nothing was found that prohibits the use of a subsatellite joined to the shuttle by a long (100 km) tether. More detailed studies directed at specific applications are recommended.


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    Title :

    Tethered subsatellite study


    Contributors:

    Publication date :

    1976-03-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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