This paper describes the application of capacitive propellant gaging techniques to the aerospace enivronment. The propellant utilization and gaging system developed for Apollo is presented. In addition, some problems peculiar to aerospace and the solutions of these problems are discussed.


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    Title :

    Propellant Gaging and Utilization for the Apollo Spacecraft


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    SAE World Congress & Exhibition ; 1964



    Publication date :

    1964-01-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :