Aerospace Materials: C17200 ROD BAR TF00
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) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| C17200 ROD BAR TF00 1.501-2.000 S | 70 | 18.5 | 18.7 | 226 | 290 | 200 | 225 | 149 | 94 | 165 | 140 | 7.3 | S | TF00 | 0.298 | 4 | Rod and bar | 0.27 | AMS 4650 and AMS 4533 | 1.501-2.000 |
| C17200 ROD BAR TF00 2.001-3.000 S | 70 | 18.5 | 18.7 | 226 | 290 | 200 | 225 | 145 | 94 | 165 | 140 | 7.3 | S | TF00 | 0.298 | 4 | Rod and bar | 0.27 | AMS 4650 and AMS 4533 | 2.001-3.000 |
| C17200 ROD BAR TF00 3.001-3.500 S | 70 | 18.5 | 18.7 | 226 | 290 | 200 | 225 | 143 | 94 | 165 | 140 | 7.3 | S | TF00 | 0.298 | 3 | Rod and bar | 0.27 | AMS 4650 and AMS 4533 | 3.001-3.500 |
| C17200 ROD BAR TF00 3.501-4.000 S | 70 | 18.5 | 18.7 | 226 | 290 | 200 | 225 | 139 | 94 | 165 | 140 | 7.3 | S | TF00 | 0.298 | 3 | Rod and bar | 0.27 | AMS 4650 and AMS 4533 | 3.501-4.000 |
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