Concept is suitable for space rendezvous missions, such as interrogation and possible negation of enemy satellites, maintenance and supply of space stations, and performance of space rescue; intermittent instrumentation of interceptor trajectory corrections; optimization procedures employed to achieve rendezvous in minimum time consistent with small fuel requirement and logic employed in system.


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    Title :

    Satellite rendezvous terminal guidance system


    Additional title:

    ARS J


    Contributors:

    Published in:

    ARS Journal ; 31 , n 11


    Publication date :

    1961


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :