Aerospace Materials: CH2 15 5PH STAINLESS STEEL BAR and FORGING BARA H1150 12 S 2 6 7 0 B C6
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) | 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 | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct ST (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 15 5PH STAINLESS STEEL BAR AND FORGING BARA H1150 12 S 2 6 7 0 B C6 | 70 | 28.5 | 29.2 | 230 | 293 | 166 | 201 | 99 | 99 | 85 | 135 | 135 | 105 | 105 | 11.2 | 50 | 35 | S | H1150 | 0.283 | 16 | 11 | Bara | 0.27 | AMS 5659 | 12 |
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