Stress area: 28.86 mm² · Proof load: 27,994 N · Clamp load (75%): 20,996 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 29.4 | 21.7 | 260.2 | 299.8 |
| Oiled | 0.15 | 22.0 | 16.2 | 194.7 | 224.3 |
| Zinc Plated | 0.18 | 26.5 | 19.5 | 234.5 | 270.2 |
| Waxed | 0.1 | 14.7 | 10.8 | 130.1 | 149.9 |
| MoS₂ | 0.12 | 17.6 | 13.0 | 155.8 | 179.5 |
| Galvanized | 0.25 | 36.7 | 27.1 | 324.8 | 374.2 |
Stress area: 31.23 mm² · Proof load: 30,293 N · Clamp load (75%): 22,720 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 31.8 | 23.5 | 281.5 | 324.3 |
| Oiled | 0.15 | 23.9 | 17.6 | 211.5 | 243.7 |
| Zinc Plated | 0.18 | 28.6 | 21.1 | 253.1 | 291.6 |
| Waxed | 0.1 | 15.9 | 11.7 | 140.7 | 162.1 |
| MoS₂ | 0.12 | 19.1 | 14.1 | 169.0 | 194.8 |
| Galvanized | 0.25 | 39.8 | 29.4 | 352.3 | 405.8 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 28.86 mm² = 20,996 N
Step 2 — Torque (dry): T = 0.20 × 0.0070 m × 20,996 N = 29.4 N·m
Proof stress per ISO 898-1:2013 Table 4. Stress area per ISO 898-1 Annex A. K-factor per VDI 2230.
Socket head cap screws, racing/motorsport, aerospace, maximum strength applications — highest standard grade