Stress area: 244.79 mm² · Proof load: 237,446 N · Clamp load (75%): 178,085 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 712.3 | 525.4 | 6304.4 | 7263.5 |
| Oiled | 0.15 | 534.3 | 394.1 | 4729.0 | 5448.4 |
| Zinc Plated | 0.18 | 641.1 | 472.9 | 5674.2 | 6537.4 |
| Waxed | 0.1 | 356.2 | 262.7 | 3152.6 | 3632.2 |
| MoS₂ | 0.12 | 427.4 | 315.2 | 3782.8 | 4358.3 |
| Galvanized | 0.25 | 890.4 | 656.7 | 7880.7 | 9079.6 |
Stress area: 271.5 mm² · Proof load: 263,355 N · Clamp load (75%): 197,516 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 790.1 | 582.7 | 6993.0 | 8056.8 |
| Oiled | 0.15 | 592.5 | 437.0 | 5244.1 | 6041.8 |
| Zinc Plated | 0.18 | 711.1 | 524.5 | 6293.8 | 7251.2 |
| Waxed | 0.1 | 395.0 | 291.3 | 3496.0 | 4027.9 |
| MoS₂ | 0.12 | 474.0 | 349.6 | 4195.3 | 4833.5 |
| Galvanized | 0.25 | 987.6 | 728.4 | 8741.0 | 10070.8 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 244.79 mm² = 178,085 N
Step 2 — Torque (dry): T = 0.20 × 0.0200 m × 178,085 N = 712.3 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