Aerospace Materials: C17200 MECH TUBE TF00 OD2.500-12.000
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 LT (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Ftu ksi LT (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| C17200 MECH TUBE TF00 OD2.500-12.000 A | 70 | 18.5 | 18.7 | 228 | 287 | 183 | 206 | 134 | 135 | 92 | 161 | 157 | 126 | 124 | 7.3 | A | TF00 | 0.298 | 3 | Mechanical tubing | 0.27 | AMS 4535 | OD2.500-12.000 | Wall0.750-2.000 |
| C17200 MECH TUBE TF00 OD2.500-12.000 B | 70 | 18.5 | 18.7 | 237 | 298 | 197 | 222 | 145 | 146 | 95 | 167 | 163 | 136 | 134 | 7.3 | B | TF00 | 0.298 | — | Mechanical tubing | 0.27 | AMS 4535 | OD2.500-12.000 | Wall0.750-2.000 |
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