Stress area: 459.41 mm² · Proof load: 445,628 N · Clamp load (75%): 334,221 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1804.8 | 1331.2 | 15973.8 | 18403.9 |
| Oiled | 0.15 | 1353.6 | 998.4 | 11980.4 | 13802.9 |
| Zinc Plated | 0.18 | 1624.3 | 1198.0 | 14376.3 | 16563.3 |
| Waxed | 0.1 | 902.4 | 665.6 | 7986.9 | 9202.0 |
| MoS₂ | 0.12 | 1082.9 | 798.7 | 9584.5 | 11042.5 |
| Galvanized | 0.25 | 2256.0 | 1663.9 | 19967.3 | 23004.9 |
Stress area: 496.18 mm² · Proof load: 481,295 N · Clamp load (75%): 360,971 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1949.2 | 1437.7 | 17251.9 | 19876.4 |
| Oiled | 0.15 | 1461.9 | 1078.2 | 12938.9 | 14907.3 |
| Zinc Plated | 0.18 | 1754.3 | 1293.9 | 15526.9 | 17888.9 |
| Waxed | 0.1 | 974.6 | 718.8 | 8625.9 | 9938.2 |
| MoS₂ | 0.12 | 1169.5 | 862.6 | 10351.0 | 11925.6 |
| Galvanized | 0.25 | 2436.6 | 1797.1 | 21565.7 | 24846.5 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 459.41 mm² = 334,221 N
Step 2 — Torque (dry): T = 0.20 × 0.0270 m × 334,221 N = 1804.8 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