Fastener calculators and formulas

Nineteen calculations that come up around screws and fasteners, from weight per thousand and thread dimensions to tightening torque and hardness conversion. Each section states the formula first, then gives a calculator that updates as you type. Every result is an estimate; acceptance and design follow the standard named on the drawing.

1. Weight per 1,000 pieces

m = V × ρ ÷ 1000

m is the mass of 1,000 pieces in kg, V the volume of one piece in mm³, and ρ the density in g/cm³. Since 1 mm³ × 1 g/cm³ = 0.001 g, the weight of one piece in grams is the weight of a thousand in kilograms. If you do not know the volume, estimate it with the next section.

Result

—kg

Weight per 1,000

Weight per piece
— g
Total weight
— kg

This is a theoretical weight. Plating, chamfers, undercuts and dimensional tolerance all move the weighed figure away from it, so use it for quoting and material planning. Counting uses a weighed average piece weight instead, for the reasons in that box of 1,000 was weighed, not counted.

2. Estimating bolt volume in segments

V = Vhead + Vshank + Vthread

Split the bolt into head, plain shank and thread, work out each, and add them; then use the total in the section above. Hexagon head V = 0.866025 × S² × K; cylindrical head V = π/4 × dk² × k; shank V = π/4 × d² × Ls; thread V = π/4 × d₂² × Lt.

Result

—kg

Weight per 1,000

Volume per piece V
— mm³
Head
— mm³
Shank
— mm³
Thread
— mm³
Pitch dia. d₂
— mm
Minor dia. d₃
— mm

The thread uses the pitch diameter, not the stress diameter

The source manual computes the thread on the stress diameter ds = (d₂+d₃)/2. This calculator defaults to the pitch diameter d₂, for the reason the same manual gives in section 8: thread rolling is a constant-volume forming process and the blank is sized on d₂. Volume before rolling equals volume after, so the threaded length weighs what a d₂ cylinder weighs. Using ds understates the thread by 9% at M10 and 10% at M3. The manual's version is kept in the menu.

A countersunk head is a frustum, not a third of a cylinder

The manual takes a countersunk head as cylinder × 1/3, which is a full cone from a point. A 90° countersunk head is a frustum from the thread diameter d out to dk, with a short cylindrical rim on top. For ISO 7046-1 M3 (dk 5.5, k 1.65) the 1/3 rule gives 13.1 mm³ and the geometry gives 27.7 mm³, half as much again. Choosing countersunk here computes the geometry, with no factor.

Pan heads still use a factor. Modelling ISO 7045 M3 (dk 5.6, k 2.4) as a cylinder with its top edge rounded to k/2 gives 0.92; the manual's 0.75 would understate an M3×10 by about 9%. The default is 0.9. The same model gives 0.867 kg per 1,000 for M3×10, against 0.876 in a published ISO 7045 weight table.

Chamfers, washer faces, cross recesses and undercuts are not included. Where accuracy matters, weigh samples and correct the factor.

3. Theoretical weight of steel sections

m = A × L × ρ ÷ 1000

A is the cross-section in mm², L the length in metres, ρ the density in g/cm³; m comes out in kg. Copper and aluminium sections use the same formula with their own density.

Result

—kg

Weight

Weight per metre
— kg/m
Cross-section A
— mm²
Weight per metre of common wire sizes (carbon steel, ρ = 7.85)
Wire dia. (mm)kg/m
5.50.187
6.50.260
80.395
100.617
120.888
141.208
161.578
202.466
253.853

Sections are made to tolerances, so this is an estimate. The angle ignores its root radius; for an exact figure use the standard section area for that size.

4. Volume of solids

Result

—mm³

Volume V

Any consistent unit works: enter mm and get mm³, enter cm and get cm³.

5. Area of plane figures

Result

—mm²

Area A

Sector and segment use the exact geometric formulas. Angles are entered in degrees.

6. Basic thread dimensions and stress area

d₂ = d − 0.64952P  d₃ = d − 1.22687P  H = 0.866025P  As = 0.7854 (d − 0.9382P)²

d₂ is the pitch diameter, d₃ the minor diameter of the external thread, and H the height of the fundamental 60° triangle. The stress area can also be written π/4 × [(d₂+d₃)/2]²; the two give the same result. As is used for tensile and proof load of external threads and does not depend on engagement length. Proof load Fp = Sp × As; minimum ultimate tensile load Fm = Rm × As.

Result

—mm²

Stress area As

Pitch dia. d₂
— mm
Minor dia. d₃
— mm
Fundamental triangle H
— mm
Proof load Fp
— kN
Min. tensile load Fm
— kN

Check: M10 × 1.5 gives As = 0.7854 × (10 − 0.9382 × 1.5)² = 58.0 mm²; at property class 10.9, Sp = 830 MPa and Fp = 830 × 58.0 = 48.1 kN.

Unified (UN) threads

As = 0.7854 (d − 0.9743 ÷ n)²

Result

—mm²

Stress area As

As
— in²
Major diameter
— mm
Pitch
— mm

7. Blank diameter before thread rolling

dblank ≈ d₂ + Δ = (d − 0.64952P) + Δ

Thread rolling is constant-volume forming: material is pushed from the root up into the crest, so the blank is sized on the pitch diameter d₂, not on the major or minor diameter. The correction Δ depends on material, die condition and tolerance class, usually 0 to +0.04 mm.

Result

—mm

Suggested blank diameter

Pitch dia. d₂
— mm
Minor dia. d₃
— mm

Too small a blank leaves the crests unfilled and the pitch diameter undersize; too large overloads the dies, splits threads and raises burrs at the crest. ISO, DIN and JIS do not specify blank diameters; the right limits move with the thread tolerance class (6g, 6h and so on in ISO 965-1) and the material, so confirm them by trial rolling before production.

8. Thread engagement percentage and pilot hole

Dhole = D − 0.6495 × P × %

Result

—mm

Suggested hole diameter

Usual engagement ranges (PSA Group standard)
Mating materialLowerUpper
Steel55%85%
Aluminium65%100%
Cast iron60%80%
Plastic50%70%

Higher engagement raises strip-out torque but also driving torque, which risks breaking or stripping the thread; for steel 70 to 75% is usual.

9. Tightening torque

T = K × d × F  F = f × Sp × As

T is the torque, K the nut factor, d the nominal diameter and F the clamp load. Clamp load is usually 60 to 75% of the proof load (the preload factor f). With d in mm and F in kN, T comes out in N·m.

Result

—N·m

Tightening torque T

Converted
— lbf·ft
Converted
— kgf·cm
Target clamp load F
— kN
Proof load Fp
— kN
Stress area As
— mm²
Reference nut factors K
Surface / treatmentKNote
Plain, unlubricated (dry)0.20The usual default
Zinc electroplated (dry)0.22Higher friction
Zinc plated + lubricant / sealer0.18—
Zinc flake coating0.15Includes a lubricating layer
Phosphate + oil0.15—
Oiled / general lubrication0.15—
Molybdenum disulphide MoS₂0.12Low friction
Stainless steel (dry)0.28Prone to galling; lubricate
Stainless steel + anti-seize0.18—

Check: M10 × 1.5, class 10.9, K = 0.20, preload factor 0.70 gives As = 58.0 mm², Fp = 48.1 kN, F = 33.7 kN and T = 0.20 × 10 × 33.7 ≈ 67 N·m.

K depends on finish, lubrication, washers and the clamped material, and is the largest source of error in this formula, up to ±30%. For critical joints, confirm with a measured torque–tension curve or the turn-of-nut method.

10. Minimum breaking torque

MBmin = τB × WP  τB = 0.6 × Rm  WP = π d₃³ ÷ 12

τB is the torsional strength, usually taken as 0.6 × Rm, and WP the plastic torsional section modulus. The test is in ISO 898-7 (DIN EN 20898-7, JIS B 1058), which covers bolts and screws M1 to M10 of property classes 8.8 to 12.9, particularly below M3, where no tensile load is specified, and parts too short (L < 2.5d) for a tensile test. It does not apply to set screws.

Result

—N·m

Minimum breaking torque

Converted
— in·lb
Minor dia. d₃
— mm
Torsional strength τB
— MPa
Section modulus WP
— mm³

Inch

Mb = d³ × UTS × 0.165

Result

—lb·in

Minimum breaking torque

Converted
— N·m

The two formulas are the same idea: 0.165 ≈ (π/12) × 0.63, the plastic section modulus times the torsion ratio. τB/Rm varies with material and heat treatment; before using it for acceptance, calibrate it against measured breaking torques.

11. Rivet length

Round head rivets

Steel L = 1.12Σδ + 1.4d  Non-ferrous L = Σδ + 1.4d

Result

—mm

Rivet length L

Grip check Σδ/d (≤ 5)
—

Countersunk rivets

A = d₀² ÷ d²  B = h(D² + D·d₀ − 2d₀²) ÷ 3d₀²  L = A·Σδ + B + C

Result

—mm

Rivet length L

A
—
B
— mm

Round L up to the nearest standard length. C depends on the rivet diameter; take it from the standard you are using.

12. Clearance holes for bolts and screws

ISO 273 (DIN EN 20273, JIS B 1001) gives fine, medium and coarse series. Fine is for high precision and reliability (aerospace, automotive, marine), medium for general machinery and structures, and coarse for undemanding equipment.

Result

—mm

Medium

Fine
— mm
Coarse
— mm
Clearance hole diameter dh (ISO 273), mm
dFineMediumCoarse
M1.61.71.82
M22.22.42.6
M2.52.72.93.1
M33.23.43.6
M44.34.54.8
M55.35.55.8
M66.46.67
M88.4910
M1010.51112
M121313.514.5
M141515.516.5
M161717.518.5
M18192021
M20212224
M22232426
M24252628
M27283032
M30313335
M33343638
M36373942
M39404245
M42434548
M45464852
M48505256

13. Hardness conversion (steel)

Enter a Vickers hardness; Brinell, Rockwell and tensile strength are interpolated linearly from the table below. Where a scale is not defined, the result shows a dash.

Result

—HRC

Rockwell C

Brinell
— HB
Rockwell B
— HRB
Tensile strength
— MPa
Conversion table (representative values, ISO 18265, ASTM E140)
HVHBHRCHRBRm (MPa)
8076—41255
10095—56320
120114—67385
140133—76450
160152—84515
180171—89575
200190—93640
220209—96705
24022820.3100770
26024724—835
28026627.1—900
30028529.8—965
32030432.2—1030
34032334.4—1095
36034236.6—1155
38036138.8—1220
40038040.8—1290
42039942.7—1350
44041844.5—1420
46043746.1—1485
480—47.7—1555
500—49.1—1595
520—50.5—1665
540—51.7—1740
560—53—1775
580—54.1—1845
600—55.2—1920
620—56.3—1995
640—57.3—2050
660—58.3—2115
680—59.3—2180
700—60.1—2240
720—61—2290
760—62.5—2400
800—64—2530
840—65.3——
900—67——
940—68——

Valid only for unalloyed and low-alloy steel and cast steel, and approximate even there; stainless steel and non-ferrous metals convert differently. For acceptance, test with the method the drawing specifies.

14. Unit conversion

Length

Result

metre m
—
millimetre mm
—
centimetre cm
—
kilometre km
—
micrometre µm
—
inch in
—
foot ft
—
yard yd
—
mile mi
—
nautical mile nmi
—
Taiwan chi (台尺)
—
Taiwan cun (台寸)
—

Mass

Result

kilogram kg
—
gram g
—
milligram mg
—
tonne t
—
pound lb
—
ounce oz
—
short ton (US)
—
long ton (UK)
—
Taiwan jin (台斤)
—
Taiwan liang (台兩)
—

Torque

Result

newton-metre N·m
—
newton-centimetre N·cm
—
kgf·m
—
kgf·cm
—
lbf·ft
—
lbf·in
—
ozf·in
—

Pressure / stress

Result

MPa (N/mm²)
—
Pa
—
kPa
—
bar
—
kgf/mm²
—
kgf/cm²
—
psi
—
ksi
—
standard atmosphere atm
—

Area

Result

square metre m²
—
square millimetre mm²
—
square centimetre cm²
—
square kilometre km²
—
square inch in²
—
square foot ft²
—
ping (坪)
—
hectare ha
—
acre
—

Volume

Result

cubic metre m³
—
cubic centimetre cm³
—
cubic millimetre mm³
—
litre L
—
millilitre mL
—
cubic inch in³
—
cubic foot ft³
—
US gallon gal
—

Temperature

Result

—°F

Fahrenheit

Kelvin
— K
Rankine
— °R

15. Densities of common materials

Density ρ (g/cm³), representative values
Materialρ (g/cm³)Note
Carbon / alloy steel7.85Common screw wire (SWRCH, 10B21, etc.)
Stainless steel 3047.93Austenitic
Stainless steel 3167.98Austenitic
Stainless steel 410 / 4207.75Martensitic
Stainless steel 4307.70Ferritic
Cast iron7.20—
Copper8.90—
Brass C360008.50—
Bronze8.80—
Aluminium / 60612.70—
Aluminium 70752.81—
Titanium TA24.51Equivalent to ASTM Grade 2
Zinc7.14—
Magnesium alloy1.80—
Nylon PA661.14—
POM1.41—

Use the value on the material certificate or specification where you have it.

16. Property classes

ISO 898-1 (DIN EN ISO 898-1, JIS B 1051); stainless per ISO 3506-1 (JIS B 1054-1)
Property classRm min (MPa)Rp0.2 min (MPa)Sp proof stress (MPa)Material
4.6400240225Low-carbon steel
4.8420340310Low-carbon steel, cold-worked
5.6500300280Low-carbon steel
5.8520420380Low-carbon steel, cold-worked
6.8600480440Medium-carbon steel
8.8 (≤ M16)800640580Medium-carbon steel, quenched and tempered
8.8 (> M16)830660600Medium-carbon steel, quenched and tempered
9.8900720650Medium-carbon steel, quenched and tempered
10.91040940830Alloy steel, quenched and tempered
12.912201100970Alloy steel, quenched and tempered
A2-70 / A4-70700450450Austenitic stainless (ISO 3506)
A2-80 / A4-80800600600Austenitic stainless (ISO 3506)

Sp is used for the proof load Fp = Sp × As.

17. ISO metric thread basic dimensions

ISO 261 (DIN 13-1, JIS B 0205); d₂, d₃ and As on the coarse pitch
SizedCoarse PFine Pd₂d₃As (mm²)
M110.25—0.8380.6930.46
M1.21.20.25—1.0380.8930.73
M1.41.40.3—1.2051.0320.98
M1.61.60.35—1.3731.1711.27
M220.4—1.7401.5092.07
M2.52.50.45—2.2081.9483.39
M330.5—2.6752.3875.03
M3.53.50.6—3.1102.7646.78
M440.7—3.5453.1418.78
M550.8—4.4804.01914.18
M6610.755.3504.77320.12
M881.2517.1886.46636.61
M10101.51.259.0268.16057.99
M12121.751.2510.8639.85384.27
M141421.512.70111.546115.44
M161621.514.70113.546156.67
M18182.51.516.37614.933192.47
M20202.51.518.37616.933244.79
M22222.51.520.37618.933303.40
M24243222.05120.319352.50
M27273225.05123.319459.41
M30303.5227.72725.706560.59
M33333.5230.72728.706693.55
M36364333.40231.093816.72
M39394336.40234.093975.75
M42424.5339.07736.4791120.91
M45454.5342.07739.4791306.01
M48485344.75241.8661473.15
M52525348.75245.8661757.84
M56565.5452.42849.2522030.02
M60605.5456.42853.2522362.02
M64646460.10356.6392675.98

The fine-pitch column lists the common value only; a size can have several fine pitches, so follow the drawing.

18. Metric and inch thread comparison

Unified threads (UN); 1 inch = 25.4 mm, pitch P = 25.4 ÷ TPI
SizeMajor (in)Major (mm)UNC TPIUNF TPIUNC pitch (mm)Nearest metric
#00.06001.524—80—M1.6
#10.07301.85464720.397M2
#20.08602.18456640.454M2
#30.09902.51548560.529M2.5
#40.11202.84540480.635M3
#50.12503.17540440.635M3
#60.13803.50532400.794M3.5
#80.16404.16632360.794M4
#100.19004.82624321.058M5
#120.21605.48624281.058M5.5
1/4"0.25006.35020281.270M6
5/16"0.31257.93818241.411M8
3/8"0.37509.52516241.587M10
7/16"0.437511.11214201.814M11
1/2"0.500012.70013201.954M12
9/16"0.562514.28712182.117M14
5/8"0.625015.87511182.309M16
3/4"0.750019.05010162.540M20
7/8"0.875022.2259142.822M22
1"1.000025.4008123.175M24
1-1/8"1.125028.5757123.629M27
1-1/4"1.250031.7507123.629M30
1-3/8"1.375034.9256124.233M36
1-1/2"1.500038.1006124.233M39
British Standard Whitworth BSW (BS 84)
SizeTPI
1/8"40
3/16"24
1/4"20
5/16"18
3/8"16
7/16"14
1/2"12
9/16"12
5/8"11
3/4"10
7/8"9
1"8

"Nearest metric" is a size comparison only. UN and metric threads have a 60° flank angle and BSW 55°; they are not interchangeable.

References

  • ISO 261, ISO general purpose metric screw threads (DIN 13-1, JIS B 0205)
  • ISO 273, clearance holes for bolts and screws (DIN EN 20273, JIS B 1001)
  • ISO 898-1, mechanical properties of carbon and alloy steel bolts, screws and studs (DIN EN ISO 898-1, JIS B 1051)
  • ISO 898-7, torsional test and minimum torques for bolts and screws, M1 to M10 (DIN EN 20898-7, JIS B 1058)
  • ISO 3506-1, mechanical properties of stainless steel fasteners (DIN EN ISO 3506-1, JIS B 1054-1)
  • ISO 7045, ISO 7046-1, cross-recessed pan and countersunk head screws (dimensions used for the pan factor and countersunk example; JIS B 1111)
  • ISO 18265, hardness conversion for metallic materials (DIN EN ISO 18265); ASTM E140
  • SAE J1701M, assembly torque for metric fasteners

Formulas and factors are compiled from the Wei Shiun Fasteners calculation handbook (20 September 2026). The two places this page departs from it, the thread diameter and the countersunk head volume, are explained in section 2.

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