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Kaiser 6033 T6, T651 Rod & Bar
Categories: Metal; Nonferrous Metal; Aluminum Alloy; 6000 Series Aluminum Alloy

Material Notes: Alloy 6033 is a higher strength version of alloy 6061, approaching properties typically obtainable with 2000 series alloys. The alloy was developed to also offer improved machinability over 6061. The improved machinability allows the user to increase speeds and feeds thus producing more parts in less time. The alloy also has shown very good corrosion resistance and excellent anodize response.

  • Ratings A through E are relative ratings in decreasing order of merit, based on exposures to sodium chloride solution by intermittent spraying or immersion. Alloys with A and B ratings can be used in industrial and seacoast atmospheres without protection. Alloys with C, D and E ratings generally should be protected at least on faying surfaces.
  • Stress-corrosion cracking ratings are based on service experience and laboratory tests of specimens exposed to the 3.5% sodium chloride alternate immersion test.
    A= No known instance of failure in service or in laboratory tests.
    B= No known instance of failure in service; limited failures in laboratory tests of short transverse specimens.
    C= Service failures with sustained tension stress acting in short transverse direction relative to grain structure; limited failures in laboratory tests of long transverse specimens.
    D= Limited service failures with sustained longitudinal or long transverse
  • Ratings A through D for Workability (cold), A through E for Machinability and A through C for Anodize Response, are relative ratings in decreasing order of merit.
  • Ratings A through D for Weldability and Brazeability are relative ratings defined as follows:
    A= Generally weldable by all commercial procedures and methods.
    B= Weldable with special techniques or for specific applications that justify preliminary trials or testing to develop welding procedure and weld performance.
    C= Limited weldability because of crack sensitivity or loss in resistance to corrosion and mechanical properties.
    D= No commonly used welding methods have been developed.

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Physical PropertiesOriginal ValueComments
Density 2.70 g/cc
 
Mechanical PropertiesOriginal ValueComments
Hardness, Brinell 120500 kg, 10 mm
Tensile Strength, Ultimate 414 MPa
@Diameter 12.7 mm
Tensile Strength, Yield 393 MPa
@Diameter 12.7 mm
Elongation at Break 13 %
@Diameter 12.7 mm
4D
Modulus of Elasticity 67.0 GPa
Shear Strength 269 MPaUltimate
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 93.45 - 97.3 %As Balance
Bismuth, Bi 0.30 - 1.0 %
Chromium, Cr <= 0.10 %
Copper, Cu 0.40 - 1.0 %
Iron, Fe <= 0.50 %
Magnesium, Mg 0.70 - 1.3 %
Manganese, Mn <= 0.050 %
Other, each <= 0.050 %
Other, total <= 0.15 %
Silicon, Si 0.80 - 1.3 %
Titanium, Ti <= 0.15 %
Zinc, Zn 0.50 - 1.0 %
 
Descriptive Properties
Anodize Response3B
Arc Weldability4A
Cold Workability3C
Gas Weldability4A
General Corrosion Resistance1B
Machinability3B
Spot Weldability4A
Stress Corrosion Resistance2A

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to go back to viewing the property data in MatWeb's normal format.

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