Stress area: 20.12 mm² · Proof load: 19,516 N · Clamp load (75%): 14,637 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 17.6 | 13.0 | 155.8 | 179.5 |
| Oiled | 0.15 | 13.2 | 9.7 | 116.8 | 134.6 |
| Zinc Plated | 0.18 | 15.8 | 11.7 | 139.8 | 161.1 |
| Waxed | 0.1 | 8.8 | 6.5 | 77.9 | 89.7 |
| MoS₂ | 0.12 | 10.5 | 7.7 | 92.9 | 107.1 |
| Galvanized | 0.25 | 22.0 | 16.2 | 194.7 | 224.3 |
Stress area: 22.03 mm² · Proof load: 21,369 N · Clamp load (75%): 16,027 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 19.2 | 14.2 | 169.9 | 195.8 |
| Oiled | 0.15 | 14.4 | 10.6 | 127.5 | 146.8 |
| Zinc Plated | 0.18 | 17.3 | 12.8 | 153.1 | 176.4 |
| Waxed | 0.1 | 9.6 | 7.1 | 85.0 | 97.9 |
| MoS₂ | 0.12 | 11.5 | 8.5 | 101.8 | 117.3 |
| Galvanized | 0.25 | 24.0 | 17.7 | 212.4 | 244.7 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 20.12 mm² = 14,637 N
Step 2 — Torque (dry): T = 0.20 × 0.0060 m × 14,637 N = 17.6 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