A configuration of the nucleonic gauging system denoted the 'Flight Test Article,' which is suitable to demonstrate gauging performance in a zero-g environment as provided by the Zero-G KC-135 aircraft flying a parabolic trajectory, was designed, fabricated, and delivered to NASA. The gauging system is projected to yield a total system accuracy of 0.25 percent of total tank capacity with a 1-second response time. This volume contains the drawings and schematic diagrams.


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    Title :

    Development of a Zero-G Gauging System. Volume II


    Contributors:
    F. E. Bupp (author)

    Publication date :

    1974


    Size :

    78 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English