Saturn/Apollo Program uses two launch vehicles, Saturn IB and Saturn V; first consists of S-IVB stage and S-IB stage while second consists of S-IVB stage, S-II stage and S-IC stage; propellant loading requirements for both vehicles are shown; elements involved in providing accurate on-board quantities of propellants are propellants sensors, storage and transfer facilities, and system to monitor sensors and control transfer; functions and operation of Propellant Tanking Computer System (PTCS) which performs propellant monitor and control function for both vehicles; electromechanical control system is designed to automatically control cryogenic propellant replenish valves using data from vehicle or ground located sensors.


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    Titel :

    Propellant tanking computer system


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Hoecker, N.L. (Autor:in) / Mathewson, J.M. (Autor:in)

    Kongress:

    SAE Meeting ; 1966 Propellants



    Erscheinungsdatum :

    1966


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    The Propellant Tanking Computer System

    Mathewson, J. M. / Hoecker, N. L. | SAE Technical Papers | 1966


    Tanking up

    Online Contents | 2001


    OTV orbital tanking systems

    Heald, D. A. / Merino, F. | NTRS | 1979



    Tanking up in China

    British Library Online Contents | 1999