Study consists of analysis and determination of propulsion requirements for each of phases of rendezvous maneuver; establishment of propulsion requirements for complete missions, representative of those which may be performed by NASA during next decade; performance of propulsion system design analysis for selected mission to establish propulsion parameters which can only be determined from design analysis; propulsion system characteristics for missions examined.


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    Title :

    Space rendezvous propulsion system requirements


    Additional title:

    Am Astronautical Soc -- Advances Astronautical Sciences


    Contributors:
    Phen, R.L. (author)


    Publication date :

    1963


    Size :

    31 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :