C17200 Copper Beryllium-TH04 Rod and bar: MIL-HDBK-5J Design Allowables
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| Material class | Beryllium |
| Alloy / temper / form | C17200 Copper Beryllium / TH04 / Rod and bar |
| Specifications | AMS 4534 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 7.3.4.0, Table 7.3.4.0(f) (pdf page 17 of the chapter file) |
| Dimension bands | 6 |
| Density | 0.298 lb/in3 |
Design Mechanical and Physical Properties (room temperature)
As printed in the handbook table. Bases: A and B are statistical minimums (99 % and 90 % probability at 95 % confidence), S the specification minimum. Grain directions: L longitudinal, LT long transverse, ST short transverse.
| Dimension band | 0.000–0.375 in | 0.376–0.999 in | 1.000–1.499 in | 1.500–1.999 in | 2.000–2.499 in | 2.500–3.000 in | |||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Specification | AMS 4534 | AMS 4534 | AMS 4534 | AMS 4534 | AMS 4534 | AMS 4534 | |||||||
| Basis | A | B | A | B | A | B | A | B | A | B | A | B | |
| Ftu, ksi | L | 182 | 188 | 180 | 186 | 177 | 184 | 177 | 183 | 175 | 181 | 172 | 178 |
| ST | … | … | … | … | … | … | 167 | 173 | 168 | 174 | 167 | 173 | |
| Fty, ksi | L | 157 | 165 | 154 | 162 | 150 | 162 | 150 | 158 | 147 | 155 | 145 | 152 |
| ST | … | … | … | … | … | … | 145 | 153 | 142 | 150 | 140 | 147 | |
| Fcy, ksi | L | … | … | 157 | 166 | 153 | 164 | 153 | 162 | 150 | 158 | 148 | 155 |
| ST | … | … | … | … | … | … | 160 | 168 | 156 | 165 | 154 | 162 | |
| Fsu, ksi | L | … | … | 89 | 92 | 91 | 95 | 94 | 97 | 95 | 98 | 94 | 96 |
| ST | … | … | … | … | … | … | 94 | 97 | 95 | 98 | 94 | 96 | |
| Fbru (e/D = 1.5), ksi | L | … | … | 242 | 250 | 238 | 247 | 238 | 246 | 235 | 243 | 231 | 239 |
| ST | … | … | … | … | … | … | 238 | 246 | 235 | 243 | 231 | 239 | |
| Fbru (e/D = 2.0), ksi | L | … | … | 306 | 317 | 302 | 313 | 302 | 312 | 298 | 308 | 293 | 303 |
| ST | … | … | … | … | … | … | 302 | 312 | 298 | 308 | 293 | 303 | |
| Fbry (e/D = 1.5), ksi | L | … | … | 220 | 231 | 214 | 228 | 214 | 226 | 210 | 221 | 207 | 217 |
| ST | … | … | … | … | … | … | 214 | 226 | 210 | 221 | 207 | 217 | |
| Fbry (e/D = 2.0), ksi | L | … | … | 239 | 251 | 233 | 248 | 233 | 245 | 228 | 240 | 225 | 236 |
| ST | … | … | … | … | … | … | 233 | 245 | 228 | 240 | 225 | 236 | |
| E, Msi | 18.5 | 18.5 | 18.5 | 18.5 | 18.5 | 18.5 | 18.5 | 18.5 | 18.5 | 18.5 | 18.5 | 18.5 | |
| Ec, Msi | 18.7 | 18.7 | 18.7 | 18.7 | 18.7 | 18.7 | 18.7 | 18.7 | 18.7 | 18.7 | 18.7 | 18.7 | |
| G, Msi | 7.3 | 7.3 | 7.3 | 7.3 | 7.3 | 7.3 | 7.3 | 7.3 | 7.3 | 7.3 | 7.3 | 7.3 | |
| ν | 0.27 | 0.27 | 0.27 | 0.27 | 0.27 | 0.27 | 0.27 | 0.27 | 0.27 | 0.27 | 0.27 | 0.27 | |
| ρ, lb/in3 | 0.298 | 0.298 | 0.298 | 0.298 | 0.298 | 0.298 | 0.298 | 0.298 | 0.298 | 0.298 | 0.298 | 0.298 | |
Effect of Temperature
The handbook maps no temperature-effect figure to this table.
Other C17200 Copper Beryllium Tables
- C17200 Copper Beryllium-TF00 Rod and bar (Table 7.3.2.0(d))
- C17200 Copper Beryllium-TH04 Rod and bar (Table 7.3.2.0(e))
Source and Use
U.S. Department of Defense (2003). Metallic Materials and Elements for Aerospace Vehicle Structures. MIL-HDBK-5J, 31 January 2003 (public domain). The values are the handbook's design allowables as extracted from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ. No warranty is given.