Stress area: 84.27 mm² · Proof load: 81,742 N · Clamp load (75%): 61,306 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 147.1 | 108.5 | 1301.9 | 1500.0 |
| Oiled | 0.15 | 110.4 | 81.4 | 977.1 | 1125.8 |
| Zinc Plated | 0.18 | 132.4 | 97.7 | 1171.8 | 1350.1 |
| Waxed | 0.1 | 73.6 | 54.3 | 651.4 | 750.5 |
| MoS₂ | 0.12 | 88.3 | 65.1 | 781.5 | 900.4 |
| Galvanized | 0.25 | 183.9 | 135.6 | 1627.7 | 1875.3 |
Stress area: 92.07 mm² · Proof load: 89,308 N · Clamp load (75%): 66,981 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 160.8 | 118.6 | 1423.2 | 1639.7 |
| Oiled | 0.15 | 120.6 | 88.9 | 1067.4 | 1229.8 |
| Zinc Plated | 0.18 | 144.7 | 106.7 | 1280.7 | 1475.5 |
| Waxed | 0.1 | 80.4 | 59.3 | 711.6 | 819.9 |
| MoS₂ | 0.12 | 96.5 | 71.2 | 854.1 | 984.0 |
| Galvanized | 0.25 | 200.9 | 148.2 | 1778.1 | 2048.6 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 84.27 mm² = 61,306 N
Step 2 — Torque (dry): T = 0.20 × 0.0120 m × 61,306 N = 147.1 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