Aerospace Materials: CH2 CUSTOM 455 STAINLESS STEEL BAR H1000 8 000 S 2 6 4 0 B C5
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 LT (ksi) | Fcy ksi ST (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 CUSTOM 455 STAINLESS STEEL BAR H1000 8 000 S 2 6 4 0 B C5 | 70 | 28.5 | 324 | 409 | 285 | 343 | 193 | 193 | 193 | 124 | 200 | 185 | 40 | S | H1000 | 0.28 | 10 | Bar | AMS 5617 | 8.000 |
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