Aerospace Materials: CH2 CUSTOM 465 STAINLESS STEEL BAR BAR H1000 12 000 A 2 6 5 0 D 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 | 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) | G Msi (Msi) | RA pct (%) | RA pct ST (%) | basis | condition | elongation pct (%) | elongation pct ST (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 CUSTOM 465 STAINLESS STEEL BAR BAR H1000 12 000 A 2 6 5 0 D C3 | 70 | 333 | 428 | 294 | 353 | 210 | 211 | 129 | 220 | 220 | 200 | 200 | 28.7 | 50 | 40 | A | H1000 | 10 | 10 | Bar | AMS 5936 | 12.000 |
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