Stress area: 5.03 mm² · Proof load: 4,879 N · Clamp load (75%): 3,659 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 2.2 | 1.6 | 19.5 | 22.4 |
| Oiled | 0.15 | 1.6 | 1.2 | 14.2 | 16.3 |
| Zinc Plated | 0.18 | 2.0 | 1.5 | 17.7 | 20.4 |
| Waxed | 0.1 | 1.1 | 0.8 | 9.7 | 11.2 |
| MoS₂ | 0.12 | 1.3 | 1.0 | 11.5 | 13.3 |
| Galvanized | 0.25 | 2.7 | 2.0 | 23.9 | 27.5 |
Stress area: 5.61 mm² · Proof load: 5,442 N · Clamp load (75%): 4,081 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 2.4 | 1.8 | 21.2 | 24.5 |
| Oiled | 0.15 | 1.8 | 1.3 | 15.9 | 18.4 |
| Zinc Plated | 0.18 | 2.2 | 1.6 | 19.5 | 22.4 |
| Waxed | 0.1 | 1.2 | 0.9 | 10.6 | 12.2 |
| MoS₂ | 0.12 | 1.5 | 1.1 | 13.3 | 15.3 |
| Galvanized | 0.25 | 3.1 | 2.3 | 27.4 | 31.6 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 5.03 mm² = 3,659 N
Step 2 — Torque (dry): T = 0.20 × 0.0030 m × 3,659 N = 2.2 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