Stress area: 352.5 mm² · Proof load: 341,925 N · Clamp load (75%): 256,444 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1230.9 | 907.9 | 10894.4 | 12551.7 |
| Oiled | 0.15 | 923.2 | 680.9 | 8171.0 | 9414.1 |
| Zinc Plated | 0.18 | 1107.8 | 817.1 | 9804.9 | 11296.5 |
| Waxed | 0.1 | 615.5 | 454.0 | 5447.6 | 6276.4 |
| MoS₂ | 0.12 | 738.6 | 544.8 | 6537.2 | 7531.7 |
| Galvanized | 0.25 | 1538.7 | 1134.9 | 13618.6 | 15690.4 |
Stress area: 384.42 mm² · Proof load: 372,887 N · Clamp load (75%): 279,666 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1342.4 | 990.1 | 11881.2 | 13688.7 |
| Oiled | 0.15 | 1006.8 | 742.6 | 8910.9 | 10266.5 |
| Zinc Plated | 0.18 | 1208.2 | 891.1 | 10693.5 | 12320.3 |
| Waxed | 0.1 | 671.2 | 495.1 | 5940.6 | 6844.4 |
| MoS₂ | 0.12 | 805.4 | 594.0 | 7128.4 | 8212.8 |
| Galvanized | 0.25 | 1678.0 | 1237.6 | 14851.6 | 17110.9 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 352.5 mm² = 256,444 N
Step 2 — Torque (dry): T = 0.20 × 0.0240 m × 256,444 N = 1230.9 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