Program determines if rendezvous in near space is possible, and performs an analysis to determine the approximate required values of the magnitude and direction of two thrust applications of the upper stage of a rocket firing. The analysis is performed by using ordinary Keplerian mechanics.


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    Title :

    Fortran 4 program for two-impulse rendezvous analysis


    Contributors:

    Publication date :

    1967-12-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





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