Stress area: 693.55 mm² · Proof load: 672,744 N · Clamp load (75%): 504,558 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 3330.1 | 2456.2 | 29473.9 | 33957.7 |
| Oiled | 0.15 | 2497.6 | 1842.1 | 22105.6 | 25468.5 |
| Zinc Plated | 0.18 | 2997.1 | 2210.5 | 26526.6 | 30562.0 |
| Waxed | 0.1 | 1665.0 | 1228.0 | 14736.5 | 16978.3 |
| MoS₂ | 0.12 | 1998.0 | 1473.6 | 17683.8 | 20374.0 |
| Galvanized | 0.25 | 4162.6 | 3070.2 | 36842.1 | 42446.9 |
Stress area: 760.85 mm² · Proof load: 738,024 N · Clamp load (75%): 553,518 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 3653.2 | 2694.5 | 32333.6 | 37252.4 |
| Oiled | 0.15 | 2739.9 | 2020.8 | 24250.2 | 27939.3 |
| Zinc Plated | 0.18 | 3287.9 | 2425.0 | 29100.4 | 33527.4 |
| Waxed | 0.1 | 1826.6 | 1347.2 | 16166.8 | 18626.2 |
| MoS₂ | 0.12 | 2191.9 | 1616.7 | 19400.0 | 22351.2 |
| Galvanized | 0.25 | 4566.5 | 3368.1 | 40416.9 | 46565.5 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 693.55 mm² = 504,558 N
Step 2 — Torque (dry): T = 0.20 × 0.0330 m × 504,558 N = 3330.1 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