A literature survey was made to determine what materials could be used to cement a thermocouple to stainless steel tubing used in the nozzle of a nuclear rocket engine. Environments included temperature and pressure excursions ranging from -424 degree f to 2000 degree f, and pressure differentials up to 750 psi.


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    Titel :

    Thermocouple cements for nuclear rocket engine nozzles


    Beteiligte:
    Barron, S. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1969


    Format / Umfang :

    5 Seiten, 6 Bilder, 2 Tabellen, 9 Quellen


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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