An optimal spacecraft trajectory correction method is examined. The method consists of determining the optimal energetics and strategy for interplanetary spacecraft trajectory correction. Calculations for the Earth-Jupiter flight trajectory are presented. (Author)


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    Title :

    Method of Determining Optimal Spacecraft Trajectory Correction


    Contributors:

    Publication date :

    1974


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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