Technique presents method of achieving orbital rendezvous because of large time tolerances on launching, low energy requirements, and relatively long times of closing during which corrective measures may be taken; errors in initial orbital establishment may be monitored and reduced by either ground or vehicle equipment; applicability to any orbital rendezvous, including moon or planets, or to position placement such as 24-hr satellites, if Earth launched point is at latitude equal to or less than orbital inclination in degrees.


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    Title :

    Phasing technique in rendezvous


    Additional title:

    ARS J


    Contributors:

    Published in:

    ARS Journal ; 32 , n 4


    Publication date :

    1962


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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