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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Thermocouple cements for nuclear rocket engine nozzles


    Contributors:
    Barron, S. (author)

    Published in:

    Publication date :

    1969


    Size :

    5 Seiten, 6 Bilder, 2 Tabellen, 9 Quellen


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Advanced Rocket Engine Nozzles

    Dumnov, G. E. / Nikulin, G. Z. / Ponomarev, N. B. et al. | British Library Conference Proceedings | 1996


    Advanced rocket engine nozzles

    Dumnov, G. / Nikulin, G. / Ponomarev, N. | AIAA | 1996




    Materials for Nuclear Rocket Nozzles

    C. W. Funk / W. Weleff | NTIS | 1965