TABLE I CHEMICAL COMPOSITIONS OF MATERIALS USED
- | C | Si | Mn | P | S | Ni | Cr | Mo | Cu | N | O | Fe |
SUS304L | .017 | .56 | .87 | .03 | .002 | 9.05 | 18.33 | .17 | .24 | .04 | .003 | Bal. |
SUS316L | .022 | .52 | .87 | .03 | .001 | 12.09 | 17.59 | 2.13 | .28 | .04 | .002 | Bal. |
- | Si | Fe | Mn | Mg | Cr | Ti | O | Al |
A5083 | - | .19 | .64 | 4.82 | .06 | .01 | .01 | Bal. |
FIGURE 2 STRESS-STRAIN CURVES OF A5083 ALUMINUM ALLOY IN LIQUID HELIUM AND HYDROGEN.
FIGURE 3 STRESS-STRAIN CURVES OF SUS304L PLATES IN LIQUID HELIUM, HYDROGEN AND NITROGEN, AND AT AMBIENT TEMPERATURE IN AIR.
FIGURE 4 STRESS-STRAIN CURVES OF SUS316L PLATES IN LIQUID HELIUM, HYDROGEN AND NITROGEN, AND AT AMBIENT TEMPERATURE IN AIR.
FIGURE 5 STRESS-STRAIN CURVES OF SUS304L AND SUS316L WELD METALS IN LIQUID HYDROGEN.
FIGURE 6 TENSILE PROPERTIES OF SUS304L THICK PLATE AS A FUNCTION OF TEST TEMPERATURE.
FIGURE 7 TENSILE PROPERTIES OF SUS316L THICK PLATE AS A FUNCTION OF TEST TEMPERATURE.