Abstract We consider the problems of control of the angular and trajectory motion of the Kliper re-entry vehicle. This spacecraft with a moderate hypersonic lift-to-drag ratio is designed according to the load-carrying frame scheme. Gas-dynamic engines, a split balancing flap, and an air brake are used as mounting devices of control.


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    Title :

    Problems of control of a re-entry vehicle with a moderate lift-to-drag ratio during its entry into the atmosphere


    Contributors:

    Published in:

    Cosmic Research ; 46 , 1 ; 74-89


    Publication date :

    2008-02-01


    Size :

    16 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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