Motion of planets in relation to each other, and conditions for attaining orbits of artificial satellites and trajectories of space probes are considered; 3- and n-body problems and their periodic solutions are briefly discussed; basic equations are given for rocket propulsion; first determination of trajectory based on vector of trajectorial velocity, importance of trajectory corrections, difficulties of trajectory to moon, and requirements for traveling to nearby planets are discussed. (See also v 106 n 13 May (I) 1964 p 545-51)


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    Title :

    Physical and astronomical principles of satellite and space flight


    Additional title:

    Physikalische und astronomische Grundlagen des Satelliten- und des Welgraumflugs


    Contributors:

    Published in:

    Publication date :

    1964


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :




    Infrared astronomical satellite

    Aumann, H.H. / Walker, R.G. | Tema Archive | 1977