Aerospace Materials: INCONEL 625 BAR ANN
Aerospace material mechanical properties and design allowables at ambient, elevated, and cryogenic temperatures per MMPDS-11 (Metallic Materials Properties Development and Standardization). Covers primary structural alloys: aluminum (2024-T3, 7075-T6, 6061-T6, 2219-T87), titanium (Ti-6Al-4V), nickel superalloys (Inconel 718), and steels (300M, 4130, 4340).
| material id | temp f | E Msi (Msi) | Ec Msi (Msi) | Fbru ksi (ksi) | Fbru ksi 2 (ksi) | Fbry ksi (ksi) | Fbry ksi 2 (ksi) | Fcy ksi (ksi) | Fcy ksi ST (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Ftu ksi ST (ksi) | Fty ksi (ksi) | Fty ksi ST (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| INCONEL 625 BAR ANN 0.500-0.999 S | 70 | 29.8 | 29.8 | 192 | 234 | 88 | 102 | 60 | — | 79 | 120 | — | 60 | — | 11.8 | S | Annealed | 0.305 | 30 | Bar | 0.28 | AMS 5666 | 0.500-0.999 |
| INCONEL 625 BAR ANN 1.000-1.999 S | 70 | 29.8 | 29.8 | 192 | 234 | 88 | 102 | 59 | — | 79 | 120 | — | 60 | — | 11.8 | S | Annealed | 0.305 | 30 | Bar | 0.28 | AMS 5666 | 1.000-1.999 |
| INCONEL 625 BAR ANN 2.000-2.999 S | 70 | 29.8 | 29.8 | 192 | 234 | 88 | 102 | 56 | 60 | 79 | 120 | 118 | 60 | 57 | 11.8 | S | Annealed | 0.305 | 30 | Bar | 0.28 | AMS 5666 | 2.000-2.999 |
| INCONEL 625 BAR ANN 3.000-3.999 S | 70 | 29.8 | 29.8 | 192 | 234 | 88 | 102 | 53 | 60 | 79 | 120 | 118 | 60 | 57 | 11.8 | S | Annealed | 0.305 | 30 | Bar | 0.28 | AMS 5666 | 3.000-3.999 |
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