It is shown, that minimum drive impulse needed for transition is obtained by applying it in moment of contact with braking ellipse.


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    Title :

    Transition of spacecraft, subject to deceleration in planet atmosphere, into orbit of artificial planet


    Additional title:

    Perekhod kosmicheskogo apparata, tormozyashchegosya v atmosfere planety, na orbitu iskustvennogo sputnika


    Contributors:
    Il'In, V.A. (author)

    Published in:

    Publication date :

    1963


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Russian


    Keywords :



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