A typical GYROLITE spacecraft recently designed by this author is described. It is shown that, for the satellite to have a stable attitude, the spinning part must have a favorable inertia ratio.


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    Title :

    The Gyrolite: A New Generation Synchronous Satellite


    Contributors:

    Published in:

    Publication date :

    1977-11-01


    Size :

    1594266 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English