"NASA-23" denotes class of alloys resisting both embrittlement by hydrogen and corrosion. Weldable and castable and formed by such standard processes as rolling, forging, and wire drawing. Heat-treated to obtain desired combinations of strength and ductility in ranges of 100 to 180 kpsi yield strength, 120 to 200 kpsi ultimate tensile strength, and 10 to 30 percent elongation at break. Used in place of most common aerospace structural alloy, Inconel(R) 718.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Alloys For Corrosive, Hydrogen-Rich Environments


    Contributors:

    Published in:

    Publication date :

    1993-10-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    UTILIZATION OF TITANIUM AND OTHER ALLOYS IN CORROSIVE ENVIRONMENTS

    WILLIAMS, W. LEE | SAE Technical Papers | 1953



    Monitoring Technology for Automobile Corrosive Environments

    Watanabe, Hirokazu / Ueki, Mitsuhiko / Saijo, Yasuhiko et al. | SAE Technical Papers | 2015



    Monitoring Technology for Automobile Corrosive Environments

    Saijo, Yasuhiko / Ueki, Mitsuhiko / Watanabe, Hirokazu et al. | British Library Conference Proceedings | 2015