Aerospace Materials: C17200 ROD BAR TH04
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 TH04 2.000-2.499 B | 70 | 18.5 | 18.7 | 243 | 308 | 221 | 240 | 158 | 98 | 181 | 155 | 7.3 | B | TH04 | 0.298 | — | Rod and bar | 0.27 | AMS 4534 | 2.000-2.499 |
| C17200 ROD BAR TH04 2.500-3.000 A | 70 | 18.5 | 18.7 | 231 | 293 | 207 | 225 | 148 | 94 | 172 | 145 | 7.3 | A | TH04 | 0.298 | 3 | Rod and bar | 0.27 | AMS 4534 | 2.500-3.000 |
| C17200 ROD BAR TH04 2.500-3.000 B | 70 | 18.5 | 18.7 | 239 | 303 | 217 | 236 | 155 | 96 | 178 | 152 | 7.3 | B | TH04 | 0.298 | — | Rod and bar | 0.27 | AMS 4534 | 2.500-3.000 |
| C17200 ROD BAR TH04 LE0.375 A | 70 | 18.5 | 18.7 | — | — | — | — | — | — | 182 | 157 | 7.3 | A | TH04 | 0.298 | 3 | Rod and bar | 0.27 | AMS 4534 | <=0.375 |
| C17200 ROD BAR TH04 LE0.375 B | 70 | 18.5 | 18.7 | — | — | — | — | — | — | 188 | 165 | 7.3 | B | TH04 | 0.298 | — | Rod and bar | 0.27 | AMS 4534 | <=0.375 |
| C17200 ROD BAR TH04 LE0.375 S | 70 | 18.5 | 18.7 | — | — | — | — | — | — | 185 | 145 | 7.3 | S | TH04 | 0.298 | 1 | Rod and bar | 0.27 | AMS 4651 | <=0.375 |
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