The device is installed in the end of a storage cylinder, in which a liquid propulsion rocket motor assembly is housed for detection of a leak in the liquid propulsion system from outside the storage cylinder. The fuel consists of a fuel component and an oxidizing component. Leakage is indicated by use of a circular absorbent pad impregnated with N-phenylanthranilic acid on one half and with mercurous chloride on the other half. The chemicals change color when contacted by components of the fuel.


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    Titel :

    Propellant Leak Indicator


    Beteiligte:
    W. E. Knight (Autor:in) / J. E. Carroll (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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