Stress area: 192.47 mm² · Proof load: 186,696 N · Clamp load (75%): 140,022 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 504.1 | 371.8 | 4461.7 | 5140.4 |
| Oiled | 0.15 | 378.1 | 278.9 | 3346.5 | 3855.6 |
| Zinc Plated | 0.18 | 453.7 | 334.6 | 4015.6 | 4626.5 |
| Waxed | 0.1 | 252.0 | 185.9 | 2230.4 | 2569.7 |
| MoS₂ | 0.12 | 302.4 | 223.0 | 2676.5 | 3083.6 |
| Galvanized | 0.25 | 630.1 | 464.7 | 5576.9 | 6425.3 |
Stress area: 216.23 mm² · Proof load: 209,743 N · Clamp load (75%): 157,307 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 566.3 | 417.7 | 5012.2 | 5774.7 |
| Oiled | 0.15 | 424.7 | 313.2 | 3758.9 | 4330.8 |
| Zinc Plated | 0.18 | 509.7 | 375.9 | 4511.2 | 5197.5 |
| Waxed | 0.1 | 283.2 | 208.9 | 2506.5 | 2887.8 |
| MoS₂ | 0.12 | 339.8 | 250.6 | 3007.5 | 3465.0 |
| Galvanized | 0.25 | 707.9 | 522.1 | 6265.4 | 7218.6 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 192.47 mm² = 140,022 N
Step 2 — Torque (dry): T = 0.20 × 0.0180 m × 140,022 N = 504.1 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