ThyssenKrupp Aerospace ThyssenKrupp Aerospace

Other materials

Weight calculations

Aluminum sheet

Sheet or plate

The weight is easily calculated. Simply multiply the appropriate alloy density (see chart opposite) by the length, width, and thickness of the required part.

Metric density (g/cm³) x T(mm) x W(m) x L(m) = weight (kg)

Imperial density (lbs/in³) x T (in) x W (in) x L (in) = weight (lbs)

Round bar

Round bar

The weight of round bar is easily calculated. Simply multiply the appropriate alloy density (see chart opposite) by the length and diameter of the required part.

Metric density (g/cm³) x D²(mm²) x L(m) x π / 4000 = weight (kg) 

Imperial density (lbs/in³) x D² (in²)   x L (in)  x π / 4 = weight (lbs) 

square bar

Square bar

The weight of square bar is easily calculated. Simply multiply the appropriate alloy density (see chart opposite) by the length and thickness multiplied by two of the required part.

Metric density (g/cm³) x T²(mm²) x L (m)/ 1000 = weight (kg) 

Imperial density (lbs/in³) x T² (in²)  x L(in) = weight (lbs) 

flat bar

Flat bar

The weight of flat bar is easily calculated. Simply multiply the appropriate alloy density (see chart below) by the length, width, and thickness of the required part.

Metric density (g/cm³) x T (mm)  x W (mm)  x L (m)/ 1000 = weight (kg) 

Imperial density (lbs/in³) x T(in) x W (in) x L (in)  = weight (lbs) 

aluminium tube

Tube

The weight of tube is easily calculated. Simply multiply the appropriate alloy density (see chart below) by the calculation shown below of the required part.

Metric density (g/cm³) x (OD² - (OD - 2xT)²) x L x π/4000 = weight

Imperial density (lbs/in³) x (OD² - (OD - 2xT)²) x L x π/4 = weight






For imperial weight calculations certain measurements (fractions) need to be converted to decimal inches.

For an accurate calculation it is also important to allow for the rolling/drawn tolerances on section for plate, sheet, square bar and flat bar; diameter for round bar; and diameter and wall thickness for tube defined by the manufacturing specification. Please contact us for details.

Densities shown in the chart are typical and should not be construed as maximum or minimum values for specification or for final design. Data on any particular piece of material may vary from those shown herein and therefore it is necessary to refer to the actual specification.

Material Density
g/cm3 lbs/in3
Aluminium Bronze 7.53 0.272
Copper Alloys 8.94 0.323
Nickel:
Alloy 25 9.13 0.330
Alloy 75 8.37 0.302
Alloy 80A 8.19 0.296
Alloy 90 8.18 0.296
Alloy C263 8.36 0.302
Alloy 400 8.83 0.319
Alloy 625 8.44 0.305
Alloy 718 8.19 0.296
Alloy K500 8.44 0.305
Alloy X750 8.28 0.299
Alloy X 8.22 0.297
Waspalloy 8.19 0.296
L-605 (Cobolt Alloy) 9.13 0.330
MP-159 (Cobolt Alloy) 8.33 0.301
MP-35N (Cobolt Alloy) 8.44 0.304
AboutServicesProductsProcessingNewsContactTeamTalk Newsletter
About
What we do
Organisational structure
Quality / approvals
Partners
Trade Associations
Sourcing & metal pricing
Costs and cost reduction
Quick response to ad-hoc requests
Service provision
Supply chain management
3rd party logistics (3PL)
Tooling management
Defence services
Subcontract management
Specification search
Aluminium
Steel
Titanium
Other materials
Data sheets
Plate cutting
Water jet cutting
Sheet cutting
Tube cutting
Bar cutting
Sheet profiling
Painting
News
Press releases
Events / Exhibitions
TeamTalk newsletters
Contact us
Enquiry form
Register for materials handbook

© Copyright ThyssenKrupp Aerospace 2010 - All right reserved