Copper Wire Weight Calculator
Calculate copper wire weight by gauge (AWG), diameter, length, and quantity. Supports solid and stranded wire with alloy density adjustments.
About
Miscalculating copper wire weight leads to structural sag in overhead spans, underestimated shipping costs, and incorrect material procurement. This calculator applies the standard volumetric mass formula W = ρ × A × L using the density of electrolytic copper at 8,960 kg/m3 (per ASTM B258 and IEC 60228). Wire diameter is derived from the AWG formula d = 0.127 × 9236 − n39 or entered directly in millimeters. Stranded conductors use a packing factor of approximately 0.90 to account for air gaps between individual strands. The tool approximates weight assuming uniform cross-section and room-temperature density. It does not account for insulation mass, tin plating, or temperature-induced expansion.
Formulas
The wire weight is computed from the volumetric mass relationship. Total mass equals the material density multiplied by conductor cross-sectional area, total length, and number of conductors:
Where W = total weight, ρ = density of copper (8,960 kg/m3 for pure Cu, per ASTM B258), A = cross-sectional area in m2, L = length in m, and n = number of conductors.
Cross-sectional area from diameter:
AWG gauge number to diameter conversion (ASTM B258 geometric progression):
Where AWG is the American Wire Gauge number. For gauges 0, 00, 000, and 0000, substitute AWG = −1, −2, −3, −4 respectively.
For stranded conductors, multiply the calculated solid area by a packing factor k (typically 0.90 for concentric lay):
Reference Data
| AWG Gauge | Diameter mm | Area mm2 | Weight kg/km | Resistance Ω/km (20°C) | Max Current A (open air) |
|---|---|---|---|---|---|
| 0000 (4/0) | 11.684 | 107.22 | 960.7 | 0.1608 | 302 |
| 000 (3/0) | 10.405 | 85.03 | 761.8 | 0.2028 | 239 |
| 00 (2/0) | 9.266 | 67.43 | 604.2 | 0.2557 | 190 |
| 0 (1/0) | 8.251 | 53.48 | 479.2 | 0.3224 | 150 |
| 1 | 7.348 | 42.41 | 380.0 | 0.4066 | 119 |
| 2 | 6.544 | 33.63 | 301.4 | 0.5127 | 94 |
| 4 | 5.189 | 21.15 | 189.5 | 0.8152 | 59 |
| 6 | 4.115 | 13.30 | 119.2 | 1.296 | 37 |
| 8 | 3.264 | 8.366 | 74.96 | 2.061 | 24 |
| 10 | 2.588 | 5.261 | 47.14 | 3.277 | 15 |
| 12 | 2.053 | 3.309 | 29.64 | 5.211 | 9.3 |
| 14 | 1.628 | 2.081 | 18.64 | 8.286 | 5.9 |
| 16 | 1.291 | 1.309 | 11.73 | 13.17 | 3.7 |
| 18 | 1.024 | 0.823 | 7.37 | 20.95 | 2.3 |
| 20 | 0.812 | 0.518 | 4.64 | 33.31 | 1.5 |
| 22 | 0.644 | 0.326 | 2.92 | 52.96 | 0.92 |
| 24 | 0.511 | 0.205 | 1.84 | 84.22 | 0.577 |
| 26 | 0.405 | 0.129 | 1.16 | 133.9 | 0.361 |
| 28 | 0.321 | 0.0810 | 0.726 | 212.9 | 0.226 |
| 30 | 0.255 | 0.0510 | 0.457 | 338.6 | 0.142 |
| 32 | 0.202 | 0.0320 | 0.287 | 538.3 | 0.091 |
| 34 | 0.160 | 0.0201 | 0.180 | 856.0 | 0.057 |
| 36 | 0.127 | 0.0127 | 0.114 | 1361 | 0.036 |
| 38 | 0.101 | 0.00797 | 0.0714 | 2164 | 0.023 |
| 40 | 0.0799 | 0.00501 | 0.0449 | 3441 | 0.014 |