Stress area: 303.4 mm² · Proof load: 294,298 N · Clamp load (75%): 220,723 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 971.2 | 716.3 | 8595.8 | 9903.5 |
| Oiled | 0.15 | 728.4 | 537.2 | 6446.9 | 7427.6 |
| Zinc Plated | 0.18 | 874.1 | 644.7 | 7736.4 | 8913.4 |
| Waxed | 0.1 | 485.6 | 358.2 | 4297.9 | 4951.8 |
| MoS₂ | 0.12 | 582.7 | 429.8 | 5157.3 | 5941.9 |
| Galvanized | 0.25 | 1214.0 | 895.4 | 10744.8 | 12379.4 |
Stress area: 333.01 mm² · Proof load: 323,020 N · Clamp load (75%): 242,265 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1066.0 | 786.2 | 9434.9 | 10870.2 |
| Oiled | 0.15 | 799.5 | 589.7 | 7076.2 | 8152.7 |
| Zinc Plated | 0.18 | 959.4 | 707.6 | 8491.4 | 9783.2 |
| Waxed | 0.1 | 533.0 | 393.1 | 4717.4 | 5435.1 |
| MoS₂ | 0.12 | 639.6 | 471.7 | 5660.9 | 6522.1 |
| Galvanized | 0.25 | 1332.5 | 982.8 | 11793.6 | 13587.8 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 303.4 mm² = 220,723 N
Step 2 — Torque (dry): T = 0.20 × 0.0220 m × 220,723 N = 971.2 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