Aerospace Materials: CH2 CUSTOM 455 STAINLESS STEEL BAR H950 4 001 6 000 S 2 6 4 0 B C4
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) | Ftu ksi LT (ksi) | Ftu ksi ST (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | Fty ksi ST (ksi) | RA pct (%) | RA pct LT (%) | RA pct ST (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct LT (%) | elongation pct ST (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 CUSTOM 455 STAINLESS STEEL BAR H950 4 001 6 000 S 2 6 4 0 B C4 | 70 | 28.5 | 347 | 440 | 303 | 358 | 214 | 214 | 214 | 130 | 220 | 220 | 220 | 205 | 205 | 205 | 40 | 20 | 20 | S | H950 | 0.28 | 10 | 5 | 5 | Bar | AMS 5617 | 4.001-6.000 |
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