Aerospace Materials: CH2 AF1410 STEEL BAR BAR A 4 25B S 2 5 2 0 B C1
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) | RA pct (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 AF1410 STEEL BAR BAR A 4 25B S 2 5 2 0 B C1 | 70 | 29.4 | 30.9 | 334 | 435 | 269 | 300 | 223 | 141 | 235 | 215 | 60 | S | . . . . . . . . . . . a | 0.283 | 12 | Bar | AMS 6527 | 4.25b |
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