Aerospace Materials: CH2 CUSTOM 450 STAINLESS STEEL BAR BAR H1050 8 000 SA 2 6 3 0 B C3
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) | 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) | RA pct (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 CUSTOM 450 STAINLESS STEEL BAR BAR H1050 8 000 SA 2 6 3 0 B C3 | 70 | 28 | 239 | 307 | 204 | 257 | 143 | 141 | 93 | 145 | 144 | 135 | 133 | 45 | Sa | H1050 | 0.28 | 12 | Bar | AMS 5763 | 8.000 |
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