Aerospace Materials: CH2 CUSTOM 450 STAINLESS STEEL BAR BAR SOLUTION TREATED H900 H950 H1000 H1050 H1100 H1150 12 000 S 2 6 3 0 C 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) | Ftu ksi (ksi) | Ftu ksi ST (ksi) | Fty ksi (ksi) | Fty ksi ST (ksi) | RA pct (%) | RA pct ST (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct ST (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 CUSTOM 450 STAINLESS STEEL BAR BAR SOLUTION TREATED H900 H950 H1000 H1050 H1100 H1150 12 000 S 2 6 3 0 C C4 | 70 | 28 | 160 | 160 | 150 | 150 | 45 | 27 | S | Solution treated H900 H950 H1000 H1050 H1100 H1150 | 0.28 | 12 | 8 | Bar | AMS 5773 | 12.000 |
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