CalcSteel · ToolsISO 898-1 · ASTM F3125 · SAE J429Nut-factor K tableNBR 8800 · AISC pretension Tb

Bolt Torque Calculator

Tightening torque and clamp-load preload from T = K·F·d — real ISO 8.8/10.9/12.9, ASTM A325/A490 and SAE proof strengths, a nut-factor table, dual kN/lbf output, the NBR 8800 · AISC minimum pretension, live bolt shear/tension from the connection engine, free CSV/PDF export, a shareable link and one-click hand-off to the 3D editor. No login.

610 N·m152.4 kNd = 20 mmthreaded lengthM20 · ISO 10.9K = 0.20 · Sp = 830 MPa

Tightening torque

610 N·m

K±25%: 457–762 N·m

Bolt preload (clamp)

152.4 kN

34,257 lbf

Tensile stress area Aₛ

244.8 mm²

proof 203.2 kN

Proof / yield load

203.2 kN

yield 220.3 kN

How this torque is built — T = K · F · d

Aₛ = 0.7854·(d − 0.9382·P)² = 244.8 mm² (P = 2.5 mm) · engine table Aₛ = 245 mm²

Fₚ (proof) = Aₛ·Sp = 244.8·830 = 203.2 kN

F (preload) = 75%·Fₚ = 152.4 kN = 34,257 lbf

T = K·F·d = 0.20 · 152.4 kN · 20 mm = 610 N·m = 450 lbf·ft

Nut-factor scatter is real — ±25 % on K (Bickford)

Same preload, torque range: 457 N·m … 762 N·mK = 0.20 → 0.150…0.250

Same torque, preload actually installed: 121.9 kN … 203.2 kNa high real K under-tensions the joint

Bolt shear + tension capacity — live from the CalcSteel connection engine

These come straight from engine/connections/boltData — the same NBR 8800:2024 nominal strengths the 3D-editor connection design uses. Torque installs the clamp; this is what the bolt can carry. Single bolt, one shear plane.

Fnv (NBR)

450 MPa

Fnt

750 MPa

φRn — shear

71.6 kN

φRn — tension

119.3 kN

fub = 1000 MPa · Ab = 314 mm² · Aₛ = 245 mm² · φ = 0.65

Structural joints — minimum pretension Tb (NBR 8800 · AISC/RCSC)

Slip-critical and pretensioned connections do not aim for a % of proof load — the code fixes a minimum bolt tension Tb = 0.70·Fu·Aₛ per diameter. Below is that value for the two structural grades at M20, plus the K·Tb·d wrench torque (turn-of-nut and DTI are the code-preferred methods — torque is calibration-only).

ASTM A325 (≈ ISO 8.8)

Tb = 142.2 kN = 31,974 lbf

torque ≈ 569 N·m = 420 lbf·ft

ASTM A490 (≈ ISO 10.9)

Tb = 178.2 kN = 40,063 lbf

torque ≈ 713 N·m = 526 lbf·ft

Bolt torque chart — ISO 10.9 · Plain / as-received (dry) · 75% proof

SizeAₛ (mm²)Preload FTorque (N·m)Torque (lbf·ft)
20.112.5 kN1511
36.622.8 kN36.527
5836.1 kN72.253
84.352.5 kN12693
11571.9 kN201148
15797.5 kN312230
192119.8 kN431318
245152.4 kN610450
303188.9 kN831613
353219.4 kN1,053777
459286 kN1,5441,139
561349 kN2,0941,544
817508.4 kN3,6612,700

Nut factors are typical published values — real scatter is ±25 %. For critical joints, calibrate K on your actual fastener/lubricant. Torque values are guidance, not a substitute for a qualified design.

What is a bolt torque calculator?

A bolt torque calculator converts the tightening torque you apply with a wrench into the preload (the axial clamp force) it creates in the bolt — and back again. That preload is the whole point of a bolted joint: it is the tension locked into the shank that squeezes the connected parts together, keeps the joint from separating or slipping, and stops the bolt from working loose under vibration and fatigue. Torque itself is only the means of installing that preload; it is never the design objective.

The relationship both directions rest on is the short-form torque equation (also called the Motosh or nut-factor equation):

T = K · F · d

  • T — tightening torque applied to the nut or bolt head (N·m or lbf·ft);
  • K — the nut factor (a.k.a. torque coefficient), a dimensionless number that lumps together thread friction, under-head friction and the thread lead. It is dominated by surface finish and lubrication, typically 0.10–0.25;
  • F — the target preload (bolt tension, in N or lbf);
  • d — the nominal bolt diameter (m or in).

This calculator does the full chain for you. Pick the diameter (metric M or imperial UNC), the strength class, the surface condition, and the fraction of proof load you want to reach; it computes the tensile stress area, the proof and yield loads, the target preload, and the torque — all pre-solved the moment the page loads, with the answer shown in both kN and lbf for preload and both N·m and lbf·ft for torque. Unlike a generic mechanical torque app, it also carries the real proof strengths of every common bolt class and the structural minimum pretension Tb that steel design codes require for slip-critical and pretensioned connections.

The T = K·F·d formula, term by term

The full torque balance of a threaded fastener has three parts — the torque that stretches the bolt through the thread helix, the torque lost to friction on the thread flanks, and the torque lost to friction under the turning nut face:

T = F · [ (P / 2π) + (μt · rt / cosα) + μn · rn ]

where P is the thread pitch, μt and μn are the thread and under-head friction coefficients, rt and rn the effective thread and bearing radii, and α the thread half-angle. Because all of those geometric and friction terms scale with the diameter, the whole bracket collapses to a single dimensionless nut factor K times the diameter d, which is why the short form T = K·F·d works so well in practice. The catch is that K is not a friction coefficient — a "K = 0.20" joint does not have μ = 0.20. K is an empirical property of the whole fastener system: bolt, nut, washer, plating and lubricant together.

Tensile stress area Aₛ. The bolt does not resist tension on its nominal area — the threads reduce it. Design uses the tensile stress area, the area of a hypothetical round bar with a diameter halfway between the pitch and minor thread diameters:

metric:    Aₛ = 0.7854 · (d − 0.9382·P)²          (mm², P = pitch)
imperial:  Aₛ = 0.7854 · (d − 0.9743/n)²          (in², n = threads per inch)

For an M20 coarse bolt (P = 2.5 mm) this gives Aₛ = 244.8 mm² — matching the 245 mm² published in every fastener table. Every strength quantity below is Aₛ times a stress.

From stress to preload. Each class has a proof stress Sp (the stress the bolt can carry with no measurable permanent set). The proof load is Fp = Aₛ·Sp, and the target preload is a chosen fraction of it — commonly 75 % for reusable joints and up to 90 % for permanent ones (closer to the yield load Aₛ·Re). Enter that fraction and the calculator returns F, then T = K·F·d.

Bolt classes and their proof strengths

The number stamped on a bolt head is not decoration — it encodes the strength. This calculator carries the real, standardised values, not one generic curve:

ISO 898-1 property classes (metric). The two-part mark "x.y" means ultimate tensile Rm ≈ x·100 MPa and yield ≈ x·y·10 MPa:

ClassProof Sp (MPa)Yield Re (MPa)Tensile Rm (MPa)Typical use
4.6225240400mild-steel general
5.8380420520medium-duty
8.8580640800structural & machine standard
10.98309001040high-strength
12.997010801220alloy, highest grade

ASTM F3125 (the standard that absorbed the old A325 and A490) — the workhorses of North-American steel construction:

GradeProof (MPa)Tensile Fu (MPa)≈ ISO
A325585830 (120 ksi)8.8
A4908251040 (150 ksi)10.9

(For imperial A325 the tensile strength drops from 120 ksi to 105 ksi above 1-in diameter; the calculator applies that reduction automatically.)

SAE J429 (imperial, common in mechanical and automotive work): Grade 2 (Sp 379 MPa / 55 ksi), Grade 5 (585 MPa / 85 ksi ≈ ISO 8.8), Grade 8 (827 MPa / 120 ksi ≈ ISO 10.9). Grade markings are the radial lines on the head — no lines for Gr 2, three lines for Gr 5, six for Gr 8.

Switch class in the tool and every downstream number — proof load, preload, torque and the whole torque chart — updates instantly.

The nut factor K — where the scatter lives

If torque control gets a bad reputation, K is the reason. Because T = K·F·d, any error in K passes straight through to the preload: two joints torqued identically but with K differing by 25 % end up with preloads differing by 25 %. And K really does vary that much — it is set almost entirely by friction and lubrication, not by how hard you pull.

Typical published nut factors (Bickford, Introduction to the Design and Behavior of Bolted Joints; Fastenal / Machinery's Handbook):

Surface / lubricationNut factor K
Plain / as-received steel, dry0.20
Zinc-plated (electroplated)0.22
Hot-dip galvanized, dry0.25
Galvanized + wax or lube0.12
Lightly oiled0.18
Waxed · MoS₂ · PTFE anti-seize0.10

Two practical consequences:

  • Lubrication cuts the torque for the same preload roughly in half. A waxed galvanized bolt (K ≈ 0.12) needs about half the torque of the same bolt dry (K ≈ 0.25) to reach the same tension. Torque a lubricated bolt to the dry value and you will over-tension it — a common way to snap high-strength bolts.
  • Never torque a galvanized structural bolt to a plain-finish chart. Hot-dip galvanizing raises K dramatically until the nut is lubricated; that is exactly why A325/A490 assemblies ship with a waxed nut.

For anything critical, calibrate K on your own fastener–lubricant combination (a bolt-tension calibrator or a load cell in a Skidmore-Wilhelm device). The table gives a defensible starting point, not a certified value — which is also why steel codes prefer preload-verifying methods over torque, as the next section explains.

Structural bolts — minimum pretension Tb (NBR 8800 · AISC)

This is where a structural bolt torque calculator parts ways with a mechanical one. In machine design you pick a preload as a fraction of proof load. In steel construction, slip-critical and pretensioned connections have a code-mandated minimum bolt pretension Tb that must be installed regardless — it is what develops the friction (faying-surface slip resistance) that the joint is designed on.

Both NBR 8800 (Tabela 20) and the AISC 360 / RCSC specification set the same value: 70 % of the minimum tensile strength,

Tb = 0.70 · Fu · Aₛ

The calculator computes Tb for the chosen diameter for both structural grades and shows the wrench torque K·Tb·d needed to reach it. A few benchmark values it reproduces exactly:

BoltTb — A325Tb — A490
M1691 kN114 kN
M20142 kN178 kN
M24205 kN257 kN
M30326 kN408 kN
3/4 in28 kip35 kip
7/8 in39 kip49 kip
1 in51 kip64 kip

These match NBR 8800 Tabela 20 and AISC/RCSC Table 7.1 to the kilonewton.

Important: for structural work, torque is a last-resort installation method. RCSC ranks four: turn-of-the-nut, direct-tension-indicator (DTI) washers, tension-control (twist-off) bolts, and calibrated wrench. The calibrated-wrench method is the only one that uses torque, and it requires daily calibration on a bolt-tension device — with the torque set 5 % above K·Tb·d to cover scatter. Use the torque here to estimate and to sanity-check; verify the actual tension with turn-of-nut or DTIs on the real joint.

How to use this calculator

  1. Choose the thread system — metric (M coarse) or imperial (UNC) — then pick the diameter from the list. The bolt sketch redraws with the diameter dimensioned AutoCAD-style.
  2. Select the grade/class. ISO 8.8/10.9/12.9, ASTM A325/A490 or SAE Gr 2/5/8 — the proof, yield and tensile strengths load automatically.
  3. Pick the surface / lubrication to set the nut factor K. This is the single biggest lever on the torque — dry vs waxed can halve it.
  4. Set the preload target as a percentage of proof load (75 % reusable, up to 90 % permanent).
  5. Read the results — they update with no "calculate" button. The KPI strip shows the tightening torque (N·m and lbf·ft), the preload (kN and lbf), the tensile stress area and the proof/yield loads. The T = K·F·d panel shows every intermediate number.
  6. Check the structural panel for the NBR 8800 / AISC minimum pretension Tb of A325 and A490 at your diameter, and the bolt torque chart for the whole size series at your chosen class and surface — click any row to jump to that size.
  7. Read the ±25 % scatter band on the torque KPI and in the derivation — it shows both the torque range for the same preload and the preload actually installed at the same torque, so you never treat the single number as exact. Tick fine thread (metric) to see the larger Aₛ and higher preload.
  8. Open the connection-engine capacity card for the bolt's shear and tension design strength (Fnv/Fnt, φRn) pulled live from the CalcSteel connection engine, with the threads-in/out-of-plane toggle.
  9. Export, share or hand off. Download the whole chart + result strip as CSV, print → PDF the sketch and results (no watermark), copy the permalink (every input travels in the URL, so a screenshot and the link reproduce your exact bolt), or open this bolt in the 3D editor as a prefilled base-plate connection.
  10. Toggle SI ⇄ imperial at the top to flip the primary units; both systems are always shown so nothing is lost.

Assumptions and limitations

  • Torque control is inherently scattered. Even with a good K, the torque method typically holds preload only to ±25–30 %. If you need tighter control, use angle (turn-of-nut), stretch measurement, or a load-indicating method.
  • K is empirical. The table values are representative, not certified. Reused bolts, galling, dirty or damaged threads, hard vs soft washers, and temperature all move K. Calibrate for critical joints.
  • Nominal diameter, coarse thread. The tool uses the nominal d and the standard coarse pitch for Aₛ. Fine threads have a slightly larger Aₛ (and thus preload for the same stress) — check a fine-thread table if that applies.
  • Elastic behaviour assumed. Preload above ~90 % of proof load starts to yield the bolt; some methods (turn-of-nut on structural bolts) deliberately do this, but the T = K·F·d preload here is meant to stay elastic.
  • Not a joint design. This sizes the installation of one bolt. It does not check bearing, tear-out, shear, prying, fatigue or the number of bolts — that is the connection design, which you can run in the CalcSteel editor and profile pages under NBR 8800 / AISC 360.
  • Lubricant on the correct surfaces. K assumes lubrication where the standard intends it (under the turned element and on the threads). Random oil on only part of the joint invalidates the value.

Worked example

M20 · ISO 10.9 · dry (K = 0.20) · 75 % of proof load

Given

  • Diameter d = 20 mm, coarse pitch P = 2.5 mm
  • Class 10.9 → proof stress Sp = 830 MPa
  • Surface: plain / as-received, dry → nut factor K = 0.20
  • Preload target = 75 % of proof load
  1. 1. Tensile stress area

    Aₛ = 0.7854·(20 − 0.9382·2.5)²

    244.8 mm² (table 245)

  2. 2. Proof load

    Fp = Aₛ·Sp = 244.8 × 830

    203.2 kN

  3. 3. Target preload

    F = 0.75 × 203.2

    152.4 kN = 34,257 lbf

  4. 4. Tightening torque

    T = K·F·d = 0.20 × 152.4 kN × 0.020 m

    609.5 N·m = 449.6 lbf·ft

  5. 5. Structural cross-check (A490, NBR 8800 · AISC)

    Tb = 0.70·Fu·Aₛ = 0.70 × 1040 × 244.8

    178.2 kN (min pretension) → torque ≈ 713 N·m

Result

T = 610 N·m (450 lbf·ft) for 152 kN preload · code min pretension Tb = 142 kN (A325) / 178 kN (A490)

Frequently asked questions

What is the bolt torque formula?

T = K·F·d, where T is tightening torque, K is the nut factor (torque coefficient, ~0.10–0.25 depending on lubrication and finish), F is the target preload (bolt tension), and d is the nominal bolt diameter. It is the short form of the full thread-friction torque balance; because every geometric and friction term scales with diameter, they collapse into the single factor K.

Is there a bolt torque chart I can read off?

Yes — this page builds a live bolt torque chart for the class and surface you select, listing tightening torque (N·m and lbf·ft), preload and tensile stress area for the whole size series (M6–M36 or 1/2 in–1-1/2 in). Change the grade, lubrication or preload % and the entire chart updates. Click any row to load that size into the sketch and KPIs.

How much torque for an M20 10.9 bolt?

About 610 N·m (450 lbf·ft) for a dry (K = 0.20) bolt tightened to 75 % of proof load — that installs roughly 152 kN of preload. Lubricated to K = 0.12 the same 152 kN needs only about 365 N·m. Grade 8.8 needs proportionally less (its proof stress is 580 vs 830 MPa). Use the calculator to match your exact class, finish and preload target.

What is the nut factor K and how do I choose it?

K is a dimensionless coefficient that lumps thread friction, under-head friction and the thread lead into one number in T = K·F·d. It is set mainly by finish and lubrication: ~0.20 dry plain steel, 0.22 zinc-plated, 0.25 hot-dip galvanized dry, 0.10–0.12 waxed/MoS₂/PTFE. It is NOT a friction coefficient. For critical joints, calibrate K on your actual bolt/lubricant with a bolt-tension device rather than trusting a table.

Why does lubrication change the required torque so much?

Because most of the torque is spent overcoming friction, not stretching the bolt. Lower friction (lubrication) means more of the torque turns into preload, so you need much less torque for the same tension — roughly half, going from galvanized dry (K ≈ 0.25) to waxed (K ≈ 0.12). Torque a lubricated bolt to the dry value and you over-tension it and can snap it.

What preload should I target — 75% or 90% of proof load?

Use ~75 % of proof load for joints that will be disassembled and reused, and up to ~90 % (near yield) for permanent, gasketed or fatigue-critical joints where maximum clamp is wanted. Higher preload improves fatigue and loosening resistance but leaves less margin before yield. This tool lets you set any fraction from 30 % to 95 %.

How is a structural (steel-connection) bolt different from a machine bolt?

Structural slip-critical and pretensioned joints do not target a % of proof load — the code fixes a minimum bolt pretension Tb = 0.70·Fu·As (NBR 8800 Tabela 20 and AISC/RCSC Table 7.1). For example M20 A325 needs 142 kN and M20 A490 needs 178 kN. This page shows Tb and the torque to reach it for both grades at your diameter.

Can I really install structural bolts by torque?

Only as the "calibrated wrench" method, and only with daily calibration on a bolt-tension calibrator, torque set ~5% above K·Tb·d. AISC/RCSC prefer turn-of-the-nut, direct-tension-indicator (DTI) washers, or tension-control twist-off bolts, because they verify tension directly rather than inferring it from a scattered nut factor. Use the torque here to estimate and cross-check, not as the sole control.

What is the tensile stress area and why not use the nominal area?

The threads remove material, so a bolt in tension resists on the tensile stress area Aₛ = 0.7854·(d − 0.9382·P)² (metric) — the area of a bar sized between the pitch and minor thread diameters. For M20 that is 244.8 mm² vs 314 mm² nominal. All proof, yield and preload figures use Aₛ, which is why the calculator computes it first.

Does this give torque in both metric and imperial units?

Yes. Preload is always shown in kN and lbf, and torque in N·m and lbf·ft, whichever thread system you pick. The SI ⇄ imperial toggle chooses which is primary; the other stays visible so a shop in either system can read it directly.

Can I export the bolt torque chart or share my result?

Yes, free and without login or watermark. Download a CSV that carries the single-bolt result strip (Aₛ, Fp, F, T, Tb for A325/A490) plus the whole size-series torque chart for your class, surface and preload %. Print → PDF bundles the dimensioned sketch and results into one page. And every input lives in the URL, so "Copy link" produces a permalink (?sys=metric&sz=M20&g=10.9&s=dry&pc=75) that rebuilds your exact bolt — a screenshot and the link together are fully shareable.

How does this connect to the CalcSteel connection design?

Two ways. The tool shows a live bolt shear + tension capacity card (Fnv/Fnt and φRn) sourced straight from the connection engine (engine/connections/boltData) — the same AISC 360 Table J3.2 / NBR 8800:2024 tables the 3D-editor uses, not a re-typed handbook. And "Open this bolt in the 3D editor" builds a real, prefilled base-plate connection (fixed-base column + base plate whose anchors already carry your diameter and grade), ready for the full NBR 8800 / AISC 360 connection check, combinations and PDF report.

Do fine threads change the torque, and does the tool handle them?

Yes. A fine pitch removes less material, so the tensile stress area Aₛ is larger — for M20 it rises from 244.8 mm² (coarse, P = 2.5) to about 271.5 mm² (fine, P = 1.5), roughly +11 % more proof load and preload for the same stress, and proportionally more torque. Tick "fine thread" (metric sizes) to switch every downstream number and the whole chart to the fine-pitch area — a case single-curve calculators quietly ignore.

Reviewed by Eng. Rilis Rodrigues Jr. · Structural Engineer — CalcSteel·Updated