Command and communication system (CCS) consists of transponder, power amplifier and antenna system; CCS is located in S-IVB instrument unit and is capable of up-data command, down-link telemetry and turn-around ranging; description of each stage of Saturn V vehicle is presented; S-IVB is third powered stage of Saturn V vehicle and separates from Apollo spacecraft at distance of approximately 20,000 nautical mi from earth; system analysis is presented and gain margins are tabulated for up-data link, down telemetry link and RF carrier.


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    Title :

    Command and communication system


    Additional title:

    NASA SP


    Contributors:
    Reed, B. (author)

    Published in:

    Publication date :

    1965


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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