Use of capacitative manometers for sensing correct ratio of oxidizer-fuel weight in missile tanks during flight.


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    Title :

    Rocket propellant manometer system


    Additional title:

    ISA -- J


    Contributors:

    Published in:

    Publication date :

    1962


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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