Aerospace Materials: CH2 AERMET 100 STEEL BAR BAR and FORGING SOLUTION TREATED and AGED 10 000 B 2 5 3 0 B C2
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) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | basis | condition | density lb in3 (lb/in^3) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 AERMET 100 STEEL BAR BAR AND FORGING SOLUTION TREATED AND AGED 10 000 B 2 5 3 0 B C2 | 70 | 28 | 28.1 | 440 | 579 | 380 | 432 | 276 | 177 | 284 | 247 | B | Solution treated and aged | 0.285 | Bar and forging | 0.305 | AMS 6532 | 10.000 |
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