ENGINEERING TOOL

M20 Bolt Torque Chart

Target preload and tightening torque ranges (min–typ–max) for M20 bolts across six property classes and five friction states. K-factor method, basis fully disclosed.

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Torque by Property Class and Friction State

Quick answer: class 8.8 · electro zinc ≈ 373 N·m (329–439); other classes and friction states below.

ClassRp0.2 (MPa)Target preload (kN)Dry / Black
K 0.18–0.22 · N·m
Electro Zinc
K 0.15–0.2 · N·m
Hot-Dip Galv.
K 0.18–0.25 · N·m
Oiled
K 0.12–0.15 · N·m
Wax / PTFE / Anti-seize
K 0.08–0.12 · N·m
4.834058.3233
210–257
198
175–233
257
210–292
152
140–175
117
93–140
8.8640109.8439
395–483
373
329–439
483
395–549
285
263–329
220
176–263
10.9940161.2645
580–709
548
484–645
709
580–806
419
387–484
322
258–387
12.91100188.7755
679–830
641
566–755
830
679–943
490
453–566
377
302–453
A2-7045077.2309
278–340
262
232–309
340
278–386
201
185–232
154
123–185
A4-80600102.9412
370–453
350
309–412
453
370–515
268
247–309
206
165–247

Cell shows the typical value; the small line below is the range (min–max).

Fine-Thread Torque Matrix

Fine-thread series (M20 × 1.5 mm) target preload and tightening torque ranges, same basis as the coarse chart; the fine-thread stress area As follows ISO 898-1:2013 Table 6 (this page takes M20 As = 272 mm²).

ClassRp0.2 (MPa)Target preload (kN)Dry / Black
K 0.18–0.22 · N·m
Electro Zinc
K 0.15–0.2 · N·m
Hot-Dip Galv.
K 0.18–0.25 · N·m
Oiled
K 0.12–0.15 · N·m
Wax / PTFE / Anti-seize
K 0.08–0.12 · N·m
4.834064.7259
233–285
220
194–259
285
233–324
168
155–194
129
104–155
8.8640121.9487
439–536
414
366–487
536
439–609
317
292–366
244
195–292
10.9940179716
644–787
609
537–716
787
644–895
465
430–537
358
286–430
12.91100209.4838
754–922
712
628–838
922
754–1047
545
503–628
419
335–503
A2-7045085.7343
308–377
291
257–343
377
308–428
223
206–257
171
137–206
A4-80600114.2457
411–503
388
343–457
503
411–571
297
274–343
228
183–274

Cell shows the typical value; the small line below is the range (min–max).

Basis of Calculation & Sources

Torque follows the K-factor (nut factor) method T = K·D·F: D is the nominal diameter and F the target preload = 70% of Rp0.2 × thread stress area (M20 As = 245 mm²). Yield strengths are published values from ISO 898-1 (carbon/alloy steel) and ISO 3506-1 (stainless A2/A4). K follows published empirical ranges per friction condition (Machinery's Handbook; the wax/PTFE/anti-seize band K≈0.10 follows Machine Design test data). The grease/MoS₂ band (K≈0.11) nearly overlaps anti-seize and is available in the calculator instead of a separate column.

Stainless note: A2/A4 austenitic thread pairs gall easily under frictional heating. Always apply anti-seize and follow the Wax/PTFE/Anti-seize column (K≈0.10).

Boundary: this chart is a simplified K-factor estimate, not a full VDI 2230 analysis (which accounts for joint resilience, embedment and assembly method). Friction is the dominant variable — no single torque value exists without its friction state. Always follow the design specification or manufacturer torque table.

FAQ

What is the tightening torque for an M20 class 8.8 bolt?

It depends on the friction state (typical values at 70% of Rp0.2 target preload): oiled ≈ 285 N·m, electro zinc ≈ 373 N·m, hot-dip galvanized ≈ 483 N·m, dry/black ≈ 439 N·m, anti-seize ≈ 220 N·m. See the matrix above for ranges — no single torque value exists without its friction state.

What is the target preload for an M20 bolt?

At 70% of Rp0.2: class 4.8 ≈ 58.3 kN, 8.8 ≈ 109.8 kN, 10.9 ≈ 161.2 kN; stainless A2-70 ≈ 77.2 kN and A4-80 ≈ 102.9 kN.

Can I use carbon-steel torque values for stainless M20 (A2-70/A4-80)?

No. The classes have different yield strengths (A2-70 = 450 MPa, A4-80 = 600 MPa), so target preloads differ; and stainless thread pairs gall easily — always apply anti-seize and follow the Wax/PTFE/Anti-seize column (K≈0.10).

What basis are these torque values calculated on?

The K-factor method T = K·D·F with target preload = 70% of Rp0.2 × stress area (yield strengths per ISO 898-1 / ISO 3506-1 published values) and K per published empirical friction ranges. Estimated values, not assembly instructions; run a full VDI 2230 analysis for critical joints.

Related References

Disclaimer: This chart is an engineering estimation for selection and budgeting only. It does not constitute assembly instructions or acceptance criteria.

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