Alloys with high resistance to stress-corrosion cracking The data given here is for information only. This table is divided according to the type of alloy. These types are : Steel alloys, Nickel alloys, Aluminium alloys, Copper alloys and Miscellaneous alloys Table I - Steel Alloys
Alloy | Condition | Carbon steel(1000 series) Low alloy steel(4130,4340 ESTEC) (E) D6AC, H-11 Music wire(ASTM 228) HY-80 steel HY-130 steel HY-140 steel 1095 spring steel 300 series
stainless steel(unsensitised)2 400 series Ferritic stainless steel (404,430,444,etc) 21-6-9 stainless steel Carpenter 20 CB Stainless steel Carpenter 200 CB-3 stainless steel A286 stainless steel AM350 stainless steel AM355 stainless steel Almar 362 stainless steel Custom 450 stainless steel Custom 455 stainless steel 15-5 pH stainless steel PH 14-8 Mo stainless steel PH 15-7 Mo stainless steel 17-7 PH stainless
steel Nitronic 33 (3) (E) Maraging steel MARVAL X12 | Below 125 kg/mm2; (180 ksi) UTS Below 125 kg/mm2; (180 ksi) UTS (1) Below 148 kg/mm2; (210 ksi) UTS Cold drawn Quenched and tempered Quenched and tempered Quenched and tempered Quenched and tempered All
All All All All All SCT
1000(4) and above SCT 1000 and above H1000(5) and above H1000 and above H1000 and above H1000 and above CH900 and SRH950 and above (6,7) CH900 CH900 All All | 1) A small number of laboratory failures of specimens cut from plate more than 2 inches thick have been observed at 75% yield, even
within this ultimate strength range. The use of thick plate should therefore be avoided in a corrosive environment when sustained tensile stress in the short transverse direction is expected. 2) Including weldments of 304L, 316L, 321 and 347. 3) Including weldments. 4) SCT 1000 = subzero cooling and tempering at 538°C (1000F) 5) H1000 = hardened above 538C (1000F) 6) CH900 = cold worked and aged at 480C (1000;F)
7) SRH950 = solution treated and tempered at 510C (950F) (E) ESA classification - not in NASA MSFC-SPEC-522A
Table I - Nickel Alloys
Alloy | Condition | Hastelloy C Hastelloy X Incoloy 800 Incoloy 901 Incoloy 903 Inconel 600 (3) Inconel 625 Inconel 718 (3) Inconel X-750 Monel K-500 NiSpan-C 902 Rene 41 Unitemp 212 Waspaloy | All All All All All Annealed Annealed All All All All All All All
| 3) Including weldments
Table I - Aluminium Alloys
Alloy, Wrought (1,2) |
Condition | Alloy, Cast (3) | Condition | 1000 series 2011 2024,
rod bar 2219 (E) 2419 (E) 2618 3000 series 5000 series 6000 series (E) 7020 7049 7149 7050 7075 7475 | All T8 T8 T6, T8 T8 T6, T8 All All (4,5) All T6 (6) T73 T73 T73 T73 T73 | 355.0, C355.0 356.0, A356.0 357.0 B358.0 (Tens-50) 359.0 380.0, A380.0 514.0 (214) 518.0 (218) 535.0 (Almag 35) A 712.0, C 712.0 | T6 All All All All As cast As cast (5) As cast (5) As cast (5) As cast | 1) Mechanical stress relieved (TX5X or TX5XX) where possible
2) Including weldments of the weldable alloys. 3) The former designation in shown in parenthesis when significantly different. 4) High magnesium content alloys 5456, 5083 and 5086 should be used only in controlled tempers (H111, H112, H116, H117, H323, H343) for resistance to stress-corrosion cracking and exfoliation 5) Alloys with magnesium content greater than 3.0% are not recommended for high temperature application, 66C (150F) and above. 6) Excluding weldments.
(E) ESA classification - not in NASA MSFC-SPEC-522A
Table I - Copper Alloys
CDA no (1) |
Condition (% cold rolled) (2) | 110 170 172 194 195 230 422 443 510 521 619
619 688 706 725 280, 524, 606, 623, 655, 704, 710 715, (E) 917, (E) 937 | 37 AT, HT (3) AT, HT (3) 37 90 40 37 10 37 37 40(9% B phase) 40(95% B phase) 40 50 50, annealed 0 0
| 1) Copper Development Association alloy number 2) Maximum per cent cold rolled for which stress-corrosion cracking data are available 3) AT = annealed and precipitation hardened, HT = work hardened and precipitation hardened
Table I - Miscellaneous Alloys
Alloy | Condition | Beryllium, S-200C HS 25 (L605) HS 188
MP35N Titanium 3Al-2.5V Titanium 6Al-4V Titanium 13V-11Cr-3Al (E) Titanium IMI 685, IMI 829 Magnesium, M1A Magnesium, LA141 Magnesium, LAZ933 (E) Cast alloy Magnesium ELEKTRON 21 | Annealed All All All All All All All All Stabilized All T6 |
(E) ESA classification - not in NASA MSFC-SPEC-522A | |